mirror of https://github.com/ArduPilot/ardupilot
APM Planner 1.1.21
fixup config highlighting mod log scanning increase calibation timeout add tcp console port 2300 add arduinoCPP - test
This commit is contained in:
parent
af21f6b2dd
commit
5cbecce8a1
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@ -247,6 +247,7 @@
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<Compile Include="Controls\ImageLabel.Designer.cs">
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<DependentUpon>ImageLabel.cs</DependentUpon>
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</Compile>
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<Compile Include="HIL\Utils.cs" />
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<Compile Include="ResEdit.cs">
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<SubType>Form</SubType>
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</Compile>
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@ -402,6 +403,7 @@
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<DependentUpon>Splash.cs</DependentUpon>
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</Compile>
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<Compile Include="srtm.cs" />
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<Compile Include="TCPConsole.cs" />
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<Compile Include="temp.cs">
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<SubType>Form</SubType>
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</Compile>
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@ -5,6 +5,8 @@ Project("{FAE04EC0-301F-11D3-BF4B-00C04F79EFBC}") = "ArdupilotMega", "ArdupilotM
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EndProject
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Project("{FAE04EC0-301F-11D3-BF4B-00C04F79EFBC}") = "Updater", "Updater\Updater.csproj", "{E64A1A41-A5B0-458E-8284-BB63705354DA}"
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EndProject
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Project("{FAE04EC0-301F-11D3-BF4B-00C04F79EFBC}") = "ArduinoCPP", "..\..\ArduinoCPP\ArduinoCPP.csproj", "{C38A02C5-3179-4047-8DC3-945341008A74}"
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EndProject
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Global
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GlobalSection(SolutionConfigurationPlatforms) = preSolution
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Debug|Any CPU = Debug|Any CPU
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@ -41,6 +43,18 @@ Global
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{E64A1A41-A5B0-458E-8284-BB63705354DA}.Release|Win32.ActiveCfg = Release|x86
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{E64A1A41-A5B0-458E-8284-BB63705354DA}.Release|x86.ActiveCfg = Release|x86
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{E64A1A41-A5B0-458E-8284-BB63705354DA}.Release|x86.Build.0 = Release|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Debug|Any CPU.ActiveCfg = Debug|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Debug|Mixed Platforms.ActiveCfg = Debug|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Debug|Mixed Platforms.Build.0 = Debug|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Debug|Win32.ActiveCfg = Debug|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Debug|x86.ActiveCfg = Debug|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Debug|x86.Build.0 = Debug|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Release|Any CPU.ActiveCfg = Release|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Release|Mixed Platforms.ActiveCfg = Release|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Release|Mixed Platforms.Build.0 = Release|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Release|Win32.ActiveCfg = Release|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Release|x86.ActiveCfg = Release|x86
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{C38A02C5-3179-4047-8DC3-945341008A74}.Release|x86.Build.0 = Release|x86
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EndGlobalSection
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GlobalSection(SolutionProperties) = preSolution
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HideSolutionNode = FALSE
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@ -299,7 +299,7 @@ namespace ArdupilotMega
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Console.WriteLine("a = {0}, the slope of the trend line.", Math.Round(a, 2));
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Console.WriteLine("b = {0}, the intercept of the trend line.", Math.Round(b, 2));
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Console.ReadLine();
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//Console.ReadLine();
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}
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#if MAVLINK10
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@ -360,6 +360,9 @@ namespace ArdupilotMega
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break;
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case (byte)(Common.ac2modes.CIRCLE):
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mode = "Circle";
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break;
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case (byte)(Common.ac2modes.LAND):
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mode = "Land";
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break;
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default:
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mode = "Unknown";
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@ -550,13 +550,13 @@ namespace ArdupilotMega.GCSViews
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{
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if (text.Length > 0)
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{
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if (sender.GetType() == typeof(NumericUpDown))
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if (text[0].GetType() == typeof(NumericUpDown))
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{
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decimal option = (decimal)(float.Parse(Params[e.ColumnIndex, e.RowIndex].Value.ToString()));
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((NumericUpDown)text[0]).Value = option;
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((NumericUpDown)text[0]).BackColor = Color.Green;
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}
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else if (sender.GetType() == typeof(ComboBox))
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else if (text[0].GetType() == typeof(ComboBox))
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{
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int option = (int)(float.Parse(Params[e.ColumnIndex, e.RowIndex].Value.ToString()));
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((ComboBox)text[0]).SelectedIndex = option;
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@ -685,7 +685,7 @@ namespace ArdupilotMega.GCSViews
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Control[] text = this.Controls.Find(value, true);
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if (text.Length > 0)
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{
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((NumericUpDown)text[0]).BackColor = Color.FromArgb(0x43, 0x44, 0x45);
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((Control)text[0]).BackColor = Color.FromArgb(0x43, 0x44, 0x45);
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}
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}
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catch { }
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@ -3,7 +3,6 @@ using System.Collections.Generic;
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using System.ComponentModel;
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using System.Data;
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using System.Drawing;
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using System.Linq;
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using System.Text;
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using System.Windows.Forms;
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using System.Text.RegularExpressions;
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@ -591,7 +590,7 @@ namespace ArdupilotMega.GCSViews
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UploadFlash(Path.GetDirectoryName(Application.ExecutablePath) + Path.DirectorySeparatorChar + @"firmware.hex", board);
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}
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void UploadFlash(string filename, string board)
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public void UploadFlash(string filename, string board)
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{
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byte[] FLASH = new byte[1];
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StreamReader sr = null;
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@ -8,8 +8,8 @@
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{
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this.components = new System.ComponentModel.Container();
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System.ComponentModel.ComponentResourceManager resources = new System.ComponentModel.ComponentResourceManager(typeof(FlightData));
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System.Windows.Forms.DataGridViewCellStyle dataGridViewCellStyle7 = new System.Windows.Forms.DataGridViewCellStyle();
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System.Windows.Forms.DataGridViewCellStyle dataGridViewCellStyle8 = new System.Windows.Forms.DataGridViewCellStyle();
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System.Windows.Forms.DataGridViewCellStyle dataGridViewCellStyle1 = new System.Windows.Forms.DataGridViewCellStyle();
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System.Windows.Forms.DataGridViewCellStyle dataGridViewCellStyle2 = new System.Windows.Forms.DataGridViewCellStyle();
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this.contextMenuStrip1 = new System.Windows.Forms.ContextMenuStrip(this.components);
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this.goHereToolStripMenuItem = new System.Windows.Forms.ToolStripMenuItem();
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this.pointCameraHereToolStripMenuItem = new System.Windows.Forms.ToolStripMenuItem();
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@ -1217,8 +1217,8 @@
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//
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// dataGridViewImageColumn1
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//
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dataGridViewCellStyle7.Alignment = System.Windows.Forms.DataGridViewContentAlignment.MiddleCenter;
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this.dataGridViewImageColumn1.DefaultCellStyle = dataGridViewCellStyle7;
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dataGridViewCellStyle1.Alignment = System.Windows.Forms.DataGridViewContentAlignment.MiddleCenter;
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this.dataGridViewImageColumn1.DefaultCellStyle = dataGridViewCellStyle1;
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resources.ApplyResources(this.dataGridViewImageColumn1, "dataGridViewImageColumn1");
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this.dataGridViewImageColumn1.Image = global::ArdupilotMega.Properties.Resources.up;
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this.dataGridViewImageColumn1.ImageLayout = System.Windows.Forms.DataGridViewImageCellLayout.Stretch;
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//
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// dataGridViewImageColumn2
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//
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dataGridViewCellStyle8.Alignment = System.Windows.Forms.DataGridViewContentAlignment.MiddleCenter;
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this.dataGridViewImageColumn2.DefaultCellStyle = dataGridViewCellStyle8;
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dataGridViewCellStyle2.Alignment = System.Windows.Forms.DataGridViewContentAlignment.MiddleCenter;
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this.dataGridViewImageColumn2.DefaultCellStyle = dataGridViewCellStyle2;
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resources.ApplyResources(this.dataGridViewImageColumn2, "dataGridViewImageColumn2");
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this.dataGridViewImageColumn2.Image = global::ArdupilotMega.Properties.Resources.down;
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this.dataGridViewImageColumn2.ImageLayout = System.Windows.Forms.DataGridViewImageCellLayout.Stretch;
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File diff suppressed because it is too large
Load Diff
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@ -270,9 +270,11 @@ namespace ArdupilotMega.GCSViews
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System.Threading.Thread.Sleep(2000);
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SITLSEND = new UdpClient(simIP, 5501);
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}
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SetupTcpJSBSim(); // old style
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}
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SetupUDPXplanes(); // fg udp style
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SetupUDPMavLink(); // pass traffic - raw
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}
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@ -591,7 +593,7 @@ namespace ArdupilotMega.GCSViews
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if (hzcounttime.Second != DateTime.Now.Second)
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{
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Console.WriteLine("SIM hz {0}", hzcount);
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// Console.WriteLine("SIM hz {0}", hzcount);
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hzcount = 0;
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hzcounttime = DateTime.Now;
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}
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@ -660,84 +662,6 @@ namespace ArdupilotMega.GCSViews
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MavLink = new UdpClient("127.0.0.1", 14550);
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}
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/// <summary>
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/// From http://code.google.com/p/gentlenav/source/browse/trunk/Tools/XP_UDB_HILSIM/utility.cpp
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/// Converts from xplanes to fixed body ref
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/// </summary>
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/// <param name="x"></param>
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/// <param name="y"></param>
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/// <param name="z"></param>
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/// <param name="alpha"></param>
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/// <param name="beta"></param>
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public static void FLIGHTtoBCBF(ref float x, ref float y, ref float z, float alpha, float beta)
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{
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float Ca = (float)Math.Cos(alpha);
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float Cb = (float)Math.Cos(beta);
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float Sa = (float)Math.Sin(alpha);
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float Sb = (float)Math.Sin(beta);
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float X_plane = (x * Ca * Cb) - (z * Sa * Cb) - (y * Sb);
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float Y_plane = (z * Sa * Sb) - (x * Ca * Sb) - (y * Cb);
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float Z_plane = (x * Sa) + (z * Ca);
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x = X_plane;
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y = Y_plane;
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z = Z_plane;
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}
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void OGLtoBCBF(ref float x, ref float y, ref float z, float phi, float theta, float psi)
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{
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float x_NED, y_NED, z_NED;
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float Cr, Cp, Cy;
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float Sr, Sp, Sy;
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//Accelerations in X-Plane are expressed in the local OpenGL reference frame, for whatever reason.
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//This coordinate system is defined as follows (taken from the X-Plane SDK Wiki):
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// The origin 0,0,0 is on the surface of the earth at sea level at some "reference point".
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// The +X axis points east from the reference point.
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// The +Z axis points south from the reference point.
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// The +Y axis points straight up away from the center of the earth at the reference point.
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// First we shall convert from this East Up South frame, to a more conventional NED (North East Down) frame.
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x_NED = -1.0f * z;
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y_NED = x;
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z_NED = -1.0f * y;
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// Next calculate cos & sin of angles for use in the transformation matrix.
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// r, p & y subscripts stand for roll pitch and yaw.
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Cr = (float)Math.Cos(phi);
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Cp = (float)Math.Cos(theta);
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Cy = (float)Math.Cos(psi);
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Sr = (float)Math.Sin(phi);
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Sp = (float)Math.Sin(theta);
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Sy = (float)Math.Sin(psi);
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// Next we need to rotate our accelerations from the NED reference frame, into the body fixed reference frame
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// THANKS TO GEORGE M SIOURIS WHOSE "MISSILE GUIDANCE AND CONTROL SYSTEMS" BOOK SEEMS TO BE THE ONLY EASY TO FIND REFERENCE THAT
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// ACTUALLY GETS THE NED TO BODY FRAME ROTATION MATRIX CORRECT!!
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// CpCy, CpSy, -Sp | local_ax
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// SrSpCy-CrSy, SrSpSy+CrCy, SrCp | local_ay
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// CrSpCy+SrSy, CrSpSy-SrCy, CrCp | local_az
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x = (x_NED * Cp * Cy) + (y_NED * Cp * Sy) - (z_NED * Sp);
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y = (x_NED * ((Sr * Sp * Cy) - (Cr * Sy))) + (y_NED * ((Sr * Sp * Sy) + (Cr * Cy))) + (z_NED * Sr * Cp);
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z = (x_NED * ((Cr * Sp * Cy) + (Sr * Sy))) + (y_NED * ((Cr * Sp * Sy) - (Sr * Cy))) + (z_NED * Cr * Cp);
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}
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double sin(double rad)
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{
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return Math.Sin(rad);
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}
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double cos(double rad)
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{
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return Math.Cos(rad);
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}
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float oldax =0, olday =0, oldaz = 0;
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DateTime oldtime = DateTime.Now;
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#if MAVLINK10
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@ -2,11 +2,13 @@
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using System.Collections.Generic;
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using System.Text;
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using YLScsDrawing.Drawing3d;
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using ArdupilotMega.HIL;
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namespace ArdupilotMega.HIL
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{
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public class Aircraft
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public class Aircraft : Utils
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{
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Aircraft self;
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public double home_latitude = 0;
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public double home_longitude = 0;
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public double home_altitude = 0;
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@ -20,15 +22,27 @@ namespace ArdupilotMega.HIL
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public double pitch = 0.0; //# degrees
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public double roll = 0.0; //# degrees
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public double yaw = 0.0; //# degrees
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public double pitch_rate = 0.0; //# degrees/s
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public double roll_rate = 0.0; //# degrees/s
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public double yaw_rate = 0.0; //# degrees/s
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public double pDeg = 0.0; // degrees/s
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public double qDeg = 0.0; // degrees/s
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public double rDeg = 0.0; // degrees/s
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public Vector3d velocity = new Vector3d(0, 0, 0); //# m/s, North, East, Up
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public Vector3d position = new Vector3d(0, 0, 0); //# m North, East, Up
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public Vector3d accel = new Vector3d(0, 0, 0); //# m/s/s North, East, Up
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public double mass = 0.0;
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public double update_frequency = 50;//# in Hz
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public double gravity = 9.8;//# m/s/s
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public Vector3d accelerometer = new Vector3d(0, 0, -9.8);
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public Aircraft()
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{
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self = this;
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}
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public void normalise()
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{
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@ -46,7 +60,8 @@ namespace ArdupilotMega.HIL
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return angle;
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}
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public void update_position() {
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public void update_position()
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{
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//'''update lat/lon/alt from position'''
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double radius_of_earth = 6378100.0;// # in meters
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@ -56,9 +71,20 @@ namespace ArdupilotMega.HIL
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altitude = home_altitude + position.Z;
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latitude = home_latitude + dlat;
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longitude = home_longitude + dlon;
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// work out what the accelerometer would see
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double xAccel = sin(radians(self.pitch)) * cos(radians(self.roll));
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double yAccel = -sin(radians(self.roll)) * cos(radians(self.pitch));
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double zAccel = -cos(radians(self.roll)) * cos(radians(self.pitch));
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double scale = 9.81 / sqrt((xAccel * xAccel) + (yAccel * yAccel) + (zAccel * zAccel));
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xAccel *= scale;
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yAccel *= scale;
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zAccel *= scale;
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self.accelerometer = new Vector3d(xAccel, yAccel, zAccel);
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}
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const float rad2deg = (float)(180 / Math.PI);
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const float deg2rad = (float)(1.0 / rad2deg);
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}
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}
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@ -3,15 +3,105 @@ using System.Collections.Generic;
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using System.Linq;
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using System.Text;
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using YLScsDrawing.Drawing3d;
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using ArdupilotMega.HIL;
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namespace ArdupilotMega.HIL
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{
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public class Motor : Utils
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{
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const bool True = true;
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const bool False = false;
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public Motor self;
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public double angle;
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public bool clockwise;
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public double servo;
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public Motor(double angle, bool clockwise, double servo)
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{
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self = this;
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self.angle = angle;
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self.clockwise = clockwise;
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self.servo = servo;
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}
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public static Motor[] build_motors(string frame)
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{
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Motor[] motors = new HIL.Motor[8];
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frame = frame.ToLower();
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if (frame.Contains("quad") || frame.Contains("quadx"))
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{
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motors = new HIL.Motor[] {
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new Motor(90, False, 1),
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new Motor(270, False, 2),
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new Motor(0, True, 3),
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new Motor(180, True, 4),
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};
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if (frame.Contains("quadx"))
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{
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foreach (int i in range(4))
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motors[i].angle -= 45.0;
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}
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}
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else if (frame.Contains("y6"))
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{
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motors = new HIL.Motor[] {
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new Motor(60, False, 1),
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new Motor(60, True, 7),
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new Motor(180, True, 4),
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new Motor(180, False, 8),
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new Motor(-60, True, 2),
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new Motor(-60, False, 3),
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};
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}
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else if (frame.Contains("hexa") || frame.Contains("hexax"))
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{
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motors = new HIL.Motor[] {
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new Motor(0, True, 1),
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new Motor(60, False, 4),
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new Motor(120, True, 8),
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new Motor(180, False, 2),
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new Motor(240, True, 3),
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new Motor(300, False, 7),
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};
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}
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else if (frame.Contains("hexax"))
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{
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motors = new HIL.Motor[] {
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new Motor(30, False, 7),
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new Motor(90, True, 1),
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new Motor(150, False, 4),
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new Motor(210, True, 8),
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new Motor(270, False, 2),
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new Motor(330, True, 3),
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};
|
||||
}
|
||||
else if (frame.Contains("octa") || frame.Contains("octax"))
|
||||
{
|
||||
motors = new HIL.Motor[] {
|
||||
new Motor(0, True, 1),
|
||||
new Motor(180, True, 2),
|
||||
new Motor(45, False, 3),
|
||||
new Motor(135, False, 4),
|
||||
new Motor(-45, False, 7),
|
||||
new Motor(-135, False, 8),
|
||||
new Motor(270, True, 10),
|
||||
new Motor(90, True, 11),
|
||||
};
|
||||
if (frame.Contains("octax"))
|
||||
{
|
||||
foreach (int i in range(8))
|
||||
motors[i].angle += 22.5;
|
||||
}
|
||||
}
|
||||
return motors;
|
||||
}
|
||||
}
|
||||
|
||||
public class QuadCopter : Aircraft
|
||||
{
|
||||
const float ft2m = (float)(1.0 / 3.2808399);
|
||||
const float rad2deg = (float)(180 / Math.PI);
|
||||
const float deg2rad = (float)(1.0 / rad2deg);
|
||||
const float kts2fps = (float)1.68780986;
|
||||
QuadCopter self;
|
||||
|
||||
int framecount = 0;
|
||||
DateTime seconds = DateTime.Now;
|
||||
|
@ -21,6 +111,7 @@ namespace ArdupilotMega.HIL
|
|||
double hover_throttle;
|
||||
double terminal_velocity;
|
||||
double terminal_rotation_rate;
|
||||
Motor[] motors;
|
||||
|
||||
Vector3d old_position;
|
||||
|
||||
|
@ -31,16 +122,20 @@ namespace ArdupilotMega.HIL
|
|||
|
||||
DateTime last_time;
|
||||
|
||||
public QuadCopter()
|
||||
public QuadCopter(string frame = "quad")
|
||||
{
|
||||
self = this;
|
||||
|
||||
motors = Motor.build_motors(frame);
|
||||
|
||||
mass = 1.0;// # Kg
|
||||
frame_height = 0.1;
|
||||
motor_speed = new double[] { 0.0, 0.0, 0.0, 0.0 };
|
||||
motor_speed = new double[motors.Length];
|
||||
hover_throttle = 0.37;
|
||||
terminal_velocity = 30.0;
|
||||
terminal_rotation_rate = 4 * 360.0;
|
||||
|
||||
thrust_scale = (mass * gravity) / (4.0 * hover_throttle);
|
||||
thrust_scale = (mass * gravity) / (motors.Length * hover_throttle);
|
||||
|
||||
last_time = DateTime.Now;
|
||||
}
|
||||
|
@ -109,25 +204,53 @@ namespace ArdupilotMega.HIL
|
|||
delta_time = new TimeSpan(0, 0, 0, 0, 20);
|
||||
}
|
||||
|
||||
//# rotational acceleration, in degrees/s/s
|
||||
double roll_accel = (m[1] - m[0]) * 5000.0;
|
||||
double pitch_accel = (m[2] - m[3]) * 5000.0;
|
||||
double yaw_accel = -((m[2] + m[3]) - (m[0] + m[1])) * 400.0;
|
||||
// rotational acceleration, in degrees/s/s, in body frame
|
||||
double roll_accel = 0.0;
|
||||
double pitch_accel = 0.0;
|
||||
double yaw_accel = 0.0;
|
||||
double thrust = 0.0;
|
||||
|
||||
//Console.WriteLine("roll {0} {1} {2}", roll_accel, roll_rate, roll);
|
||||
foreach (var i in range((self.motors.Length)))
|
||||
{
|
||||
roll_accel += -5000.0 * sin(radians(self.motors[i].angle)) * m[i];
|
||||
pitch_accel += 5000.0 * cos(radians(self.motors[i].angle)) * m[i];
|
||||
if (self.motors[i].clockwise)
|
||||
{
|
||||
yaw_accel -= m[i] * 400.0;
|
||||
}
|
||||
else
|
||||
{
|
||||
yaw_accel += m[i] * 400.0;
|
||||
}
|
||||
thrust += m[i] * self.thrust_scale; // newtons
|
||||
}
|
||||
|
||||
// rotational resistance
|
||||
roll_accel -= (roll_rate / terminal_rotation_rate) * 5000.0;
|
||||
pitch_accel -= (pitch_rate / terminal_rotation_rate) * 5000.0;
|
||||
yaw_accel -= (yaw_rate / terminal_rotation_rate) * 400.0;
|
||||
|
||||
//# update rotational rates
|
||||
roll_rate += roll_accel * delta_time.TotalSeconds;
|
||||
pitch_rate += pitch_accel * delta_time.TotalSeconds;
|
||||
yaw_rate += yaw_accel * delta_time.TotalSeconds;
|
||||
roll_accel -= (self.pDeg / self.terminal_rotation_rate) * 5000.0;
|
||||
pitch_accel -= (self.qDeg / self.terminal_rotation_rate) * 5000.0;
|
||||
yaw_accel -= (self.rDeg / self.terminal_rotation_rate) * 400.0;
|
||||
|
||||
//Console.WriteLine("roll {0} {1} {2}", roll_accel, roll_rate, roll);
|
||||
|
||||
//# update rotational rates in body frame
|
||||
self.pDeg += roll_accel * delta_time.TotalSeconds;
|
||||
self.qDeg += pitch_accel * delta_time.TotalSeconds;
|
||||
self.rDeg += yaw_accel * delta_time.TotalSeconds;
|
||||
|
||||
// Console.WriteLine("roll {0} {1} {2}", roll_accel, roll_rate, roll);
|
||||
|
||||
// calculate rates in earth frame
|
||||
|
||||
var answer = BodyRatesToEarthRates(self.roll, self.pitch, self.yaw,
|
||||
self.pDeg, self.qDeg, self.rDeg);
|
||||
self.roll_rate = answer.Item1;
|
||||
self.pitch_rate = answer.Item2;
|
||||
self.yaw_rate = answer.Item3;
|
||||
|
||||
//self.roll_rate = pDeg;
|
||||
//self.pitch_rate = qDeg;
|
||||
//self.yaw_rate = rDeg;
|
||||
|
||||
//# update rotation
|
||||
roll += roll_rate * delta_time.TotalSeconds;
|
||||
pitch += pitch_rate * delta_time.TotalSeconds;
|
||||
|
@ -143,7 +266,6 @@ namespace ArdupilotMega.HIL
|
|||
//# normalise rotations
|
||||
normalise();
|
||||
|
||||
double thrust = (m[0] + m[1] + m[2] + m[3]) * thrust_scale;//# Newtons
|
||||
double accel = thrust / mass;
|
||||
|
||||
//Console.WriteLine("in {0:0.000000} {1:0.000000} {2:0.000000} {3:0.000000}", roll, pitch, yaw, accel);
|
||||
|
|
|
@ -0,0 +1,104 @@
|
|||
using System;
|
||||
using System.Collections.Generic;
|
||||
using System.Linq;
|
||||
using System.Text;
|
||||
|
||||
namespace ArdupilotMega.HIL
|
||||
{
|
||||
public class Utils
|
||||
{
|
||||
public const float rad2deg = (float)(180 / System.Math.PI);
|
||||
public const float deg2rad = (float)(1.0 / rad2deg);
|
||||
public const float ft2m = (float)(1.0 / 3.2808399);
|
||||
public const float kts2fps = (float)1.68780986;
|
||||
|
||||
public static double sin(double val)
|
||||
{
|
||||
return System.Math.Sin(val);
|
||||
}
|
||||
public static double cos(double val)
|
||||
{
|
||||
return System.Math.Cos(val);
|
||||
}
|
||||
public static double radians(double val)
|
||||
{
|
||||
return val * deg2rad;
|
||||
}
|
||||
public static double degrees(double val)
|
||||
{
|
||||
return val * rad2deg;
|
||||
}
|
||||
public static double sqrt(double val)
|
||||
{
|
||||
return System.Math.Sqrt(val);
|
||||
}
|
||||
|
||||
public static int[] range(int no)
|
||||
{
|
||||
int[] range = new int[no];
|
||||
for (int a = 0; a < no; a++)
|
||||
{
|
||||
range[a] = a;
|
||||
}
|
||||
return range;
|
||||
}
|
||||
|
||||
public static double fabs(double val)
|
||||
{
|
||||
return System.Math.Abs(val);
|
||||
}
|
||||
|
||||
public static double tan(double val)
|
||||
{
|
||||
return System.Math.Tan(val);
|
||||
}
|
||||
|
||||
|
||||
public static Tuple<double,double,double> EarthRatesToBodyRates(double roll,double pitch,double yaw,
|
||||
double rollRate,double pitchRate,double yawRate) {
|
||||
//convert the angular velocities from earth frame to
|
||||
//body frame. Thanks to James Goppert for the formula
|
||||
|
||||
//all inputs and outputs are in degrees
|
||||
|
||||
//returns a tuple, (p,q,r)
|
||||
|
||||
|
||||
var phi = radians(roll);
|
||||
var theta = radians(pitch);
|
||||
var phiDot = radians(rollRate);
|
||||
var thetaDot = radians(pitchRate);
|
||||
var psiDot = radians(yawRate);
|
||||
|
||||
var p = phiDot - psiDot*sin(theta);
|
||||
var q = cos(phi)*thetaDot + sin(phi)*psiDot*cos(theta);
|
||||
var r = cos(phi)*psiDot*cos(theta) - sin(phi)*thetaDot;
|
||||
|
||||
return new Tuple<double,double,double> (degrees(p), degrees(q), degrees(r));
|
||||
}
|
||||
|
||||
public static Tuple<double,double,double> BodyRatesToEarthRates(double roll, double pitch, double yaw,double pDeg, double qDeg,double rDeg){
|
||||
//convert the angular velocities from body frame to
|
||||
//earth frame.
|
||||
|
||||
//all inputs and outputs are in degrees
|
||||
|
||||
//returns a tuple, (rollRate,pitchRate,yawRate)
|
||||
|
||||
var p = radians(pDeg);
|
||||
var q = radians(qDeg);
|
||||
var r = radians(rDeg);
|
||||
|
||||
var phi = radians(roll);
|
||||
var theta = radians(pitch);
|
||||
|
||||
var phiDot = p + tan(theta)*(q*sin(phi) + r*cos(phi));
|
||||
var thetaDot = q*cos(phi) - r*sin(phi);
|
||||
if (fabs(cos(theta)) < 1.0e-20)
|
||||
theta += 1.0e-10;
|
||||
var psiDot = (q*sin(phi) + r*cos(phi))/cos(theta);
|
||||
|
||||
return new Tuple<double,double,double> (degrees(phiDot), degrees(thetaDot), degrees(psiDot));
|
||||
}
|
||||
}
|
||||
}
|
|
@ -27,6 +27,7 @@ namespace hud
|
|||
object paintlock = new object();
|
||||
object streamlock = new object();
|
||||
MemoryStream _streamjpg = new MemoryStream();
|
||||
[System.ComponentModel.Browsable(false)]
|
||||
public MemoryStream streamjpg { get { lock (streamlock) { return _streamjpg; } } set { lock (streamlock) { _streamjpg = value; } } }
|
||||
/// <summary>
|
||||
/// this is to reduce cpu usage
|
||||
|
@ -44,7 +45,10 @@ namespace hud
|
|||
public HUD()
|
||||
{
|
||||
if (this.DesignMode)
|
||||
return;
|
||||
{
|
||||
opengl = false;
|
||||
//return;
|
||||
}
|
||||
|
||||
InitializeComponent();
|
||||
|
||||
|
@ -237,7 +241,7 @@ namespace hud
|
|||
{
|
||||
e.Graphics.Clear(this.BackColor);
|
||||
e.Graphics.Flush();
|
||||
return;
|
||||
//return;
|
||||
}
|
||||
|
||||
if ((DateTime.Now - starttime).TotalMilliseconds < 30 && (_bgimage == null))
|
||||
|
@ -277,7 +281,7 @@ namespace hud
|
|||
if (DateTime.Now.Second != countdate.Second)
|
||||
{
|
||||
countdate = DateTime.Now;
|
||||
Console.WriteLine("HUD " + count + " hz drawtime " + (huddrawtime / count) + " gl " + opengl);
|
||||
// Console.WriteLine("HUD " + count + " hz drawtime " + (huddrawtime / count) + " gl " + opengl);
|
||||
if ((huddrawtime / count) > 1000)
|
||||
opengl = false;
|
||||
|
||||
|
@ -1202,19 +1206,19 @@ namespace hud
|
|||
|
||||
if (gpsfix == 0)
|
||||
{
|
||||
gps = resources.GetString("GPS: No GPS.Text");
|
||||
gps = ("GPS: No GPS");
|
||||
}
|
||||
else if (gpsfix == 1)
|
||||
{
|
||||
gps = resources.GetString("GPS: No Fix.Text");
|
||||
gps = ("GPS: No Fix");
|
||||
}
|
||||
else if (gpsfix == 2)
|
||||
{
|
||||
gps = resources.GetString("GPS: 2D Fix.Text");
|
||||
gps = ("GPS: 3D Fix");
|
||||
}
|
||||
else if (gpsfix == 3)
|
||||
{
|
||||
gps = resources.GetString("GPS: 3D Fix.Text");
|
||||
gps = ("GPS: 3D Fix");
|
||||
}
|
||||
|
||||
drawstring(graphicsObject, gps, font, fontsize + 2, whiteBrush, this.Width - 10 * fontsize, this.Height - 30 - fontoffset);
|
||||
|
|
|
@ -347,6 +347,8 @@ namespace ArdupilotMega
|
|||
|
||||
if (items.Length == 11 && items[6] == "0.0000")
|
||||
alt = double.Parse(items[7], new System.Globalization.CultureInfo("en-US"));
|
||||
if (items.Length == 11 && items[6] == "0")
|
||||
alt = double.Parse(items[7], new System.Globalization.CultureInfo("en-US"));
|
||||
|
||||
|
||||
position[positionindex].Add(new Point3D(double.Parse(items[5], new System.Globalization.CultureInfo("en-US")), double.Parse(items[4], new System.Globalization.CultureInfo("en-US")), alt));
|
||||
|
|
|
@ -974,7 +974,7 @@ namespace ArdupilotMega
|
|||
actionid == MAV_ACTION.MAV_ACTION_REBOOT)
|
||||
{
|
||||
retrys = 1;
|
||||
timeout = 6000;
|
||||
timeout = 20000;
|
||||
}
|
||||
|
||||
while (true)
|
||||
|
@ -2001,8 +2001,9 @@ namespace ArdupilotMega
|
|||
|
||||
if (temp[0] != 254 && temp[0] != 'U' || lastbad[0] == 'I' && lastbad[1] == 'M') // out of sync
|
||||
{
|
||||
if (temp[0] >= 0x20 && temp[0] <= 127 || temp[0] == '\n')
|
||||
if (temp[0] >= 0x20 && temp[0] <= 127 || temp[0] == '\n' || temp[0] == '\r')
|
||||
{
|
||||
TCPConsole.Write(temp[0]);
|
||||
Console.Write((char)temp[0]);
|
||||
}
|
||||
count = 0;
|
||||
|
|
|
@ -4,6 +4,7 @@ using System.Windows.Forms;
|
|||
using System.Net;
|
||||
using System.IO;
|
||||
using System.Text;
|
||||
using System.Threading;
|
||||
|
||||
|
||||
namespace ArdupilotMega
|
||||
|
@ -32,9 +33,7 @@ namespace ArdupilotMega
|
|||
Application.SetCompatibleTextRenderingDefault(false);
|
||||
try
|
||||
{
|
||||
|
||||
Application.Run(new MainV2());
|
||||
|
||||
}
|
||||
catch (Exception ex) { Console.WriteLine(ex.ToString()); }
|
||||
}
|
||||
|
|
|
@ -11,7 +11,7 @@ using System.Resources;
|
|||
[assembly: AssemblyConfiguration("")]
|
||||
[assembly: AssemblyCompany("Michael Oborne")]
|
||||
[assembly: AssemblyProduct("ArdupilotMega Planner")]
|
||||
[assembly: AssemblyCopyright("Copyright © Michael Oborne 2010-2011")]
|
||||
[assembly: AssemblyCopyright("Copyright © Michael Oborne 2010-2012")]
|
||||
[assembly: AssemblyTrademark("")]
|
||||
[assembly: AssemblyCulture("")]
|
||||
|
||||
|
@ -34,5 +34,5 @@ using System.Resources;
|
|||
// by using the '*' as shown below:
|
||||
// [assembly: AssemblyVersion("1.0.*")]
|
||||
[assembly: AssemblyVersion("1.0.0.0")]
|
||||
[assembly: AssemblyFileVersion("1.1.20")]
|
||||
[assembly: AssemblyFileVersion("1.1.21")]
|
||||
[assembly: NeutralResourcesLanguageAttribute("")]
|
||||
|
|
|
@ -0,0 +1,71 @@
|
|||
using System;
|
||||
using System.Collections.Generic;
|
||||
using System.Linq;
|
||||
using System.Text;
|
||||
using System.Net;
|
||||
using System.Net.Sockets;
|
||||
|
||||
namespace ArdupilotMega
|
||||
{
|
||||
static class TCPConsole
|
||||
{
|
||||
static TcpListener listener;
|
||||
static TcpClient client;
|
||||
static bool started = false;
|
||||
|
||||
static void startup()
|
||||
{
|
||||
started = true;
|
||||
try
|
||||
{
|
||||
listener = new TcpListener(IPAddress.Any, 2300);
|
||||
|
||||
listener.Start();
|
||||
|
||||
listener.BeginAcceptTcpClient(
|
||||
new AsyncCallback(DoAcceptTcpClientCallback),
|
||||
listener);
|
||||
}
|
||||
catch { Console.WriteLine("TCP Console fail: port 2300"); return; }
|
||||
|
||||
}
|
||||
|
||||
// Process the client connection.
|
||||
static void DoAcceptTcpClientCallback(IAsyncResult ar)
|
||||
{
|
||||
// Get the listener that handles the client request.
|
||||
TcpListener listener = (TcpListener)ar.AsyncState;
|
||||
|
||||
// End the operation and display the received data on
|
||||
// the console.
|
||||
client = listener.EndAcceptTcpClient(ar);
|
||||
|
||||
// setup for next listener
|
||||
listener.BeginAcceptTcpClient(
|
||||
new AsyncCallback(DoAcceptTcpClientCallback),
|
||||
listener);
|
||||
|
||||
// Process the connection here. (Add the client to a
|
||||
// server table, read data, etc.)
|
||||
Console.WriteLine("Client connected completed");
|
||||
|
||||
client.Client.NoDelay = true;
|
||||
}
|
||||
|
||||
public static void Write(byte thing)
|
||||
{
|
||||
if (!started)
|
||||
startup();
|
||||
|
||||
if (client == null)
|
||||
return;
|
||||
if (!client.Connected)
|
||||
return;
|
||||
try
|
||||
{
|
||||
client.GetStream().WriteByte(thing);
|
||||
}
|
||||
catch { }
|
||||
}
|
||||
}
|
||||
}
|
|
@ -3,5 +3,5 @@
|
|||
<configSections>
|
||||
</configSections>
|
||||
<startup useLegacyV2RuntimeActivationPolicy="true">
|
||||
</startup>
|
||||
<supportedRuntime version="v2.0.50727"/></startup>
|
||||
</configuration>
|
||||
|
|
|
@ -0,0 +1,3 @@
|
|||
<?xml version="1.0"?>
|
||||
<configuration>
|
||||
<startup><supportedRuntime version="v2.0.50727"/></startup></configuration>
|
|
@ -3,5 +3,5 @@
|
|||
<configSections>
|
||||
</configSections>
|
||||
<startup useLegacyV2RuntimeActivationPolicy="true">
|
||||
</startup>
|
||||
<supportedRuntime version="v2.0.50727"/></startup>
|
||||
</configuration>
|
||||
|
|
|
@ -51,7 +51,7 @@ namespace ArdupilotMega
|
|||
}
|
||||
catch (JpegProcessingException e)
|
||||
{
|
||||
Console.Error.WriteLine(e.Message);
|
||||
Console.WriteLine(e.Message);
|
||||
return dtaken;
|
||||
}
|
||||
|
||||
|
|
Loading…
Reference in New Issue