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fixed throttle range for motor arming, removed negative sign for roll in acro mode now that APM orientation is decided 

git-svn-id: https://arducopter.googlecode.com/svn/trunk@43 f9c3cf11-9bcb-44bc-f272-b75c42450872
This commit is contained in:
CaranchoEngineering 2010-07-14 08:22:46 +00:00
parent 8a82413080
commit c0edb56fef
1 changed files with 6 additions and 13 deletions
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19
Arducopter/Arducopter.pde
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@ -323,14 +323,7 @@ void Rate_control()
float currentRollRate, currentPitchRate, currentYawRate;
// ROLL CONTROL
// NOTE: We need to test THIS !! Plaese CHECK
#ifdef FLIGHT_MODE_+
currentRollRate = read_adc(0); // I need a positive sign here
#endif
#ifdef FLIGHT_MODE_X
currentRollRate = -read_adc(0); // Original from Ted
#endif
currentRollRate = read_adc(0); // I need a positive sign here
err_roll = ((ch_roll-1500) * xmitFactor) - currentRollRate;
@ -699,7 +692,7 @@ void loop(){
command_rx_yaw_diff = 0;
}
// Arm motor output
if (ch_throttle < 1100) {
if (ch_throttle < 1200) {
control_yaw = 0;
if (ch_yaw > 1800)
motorArmed = 1;
@ -719,10 +712,10 @@ void loop(){
backMotor = ch_throttle - control_pitch + control_yaw;
#endif
#ifdef FLIGHT_MODE_X
frontMotor = ch_throttle + control_roll - control_pitch - control_yaw; // front left motor
rightMotor = ch_throttle - control_roll - control_pitch + control_yaw; // front right motor
leftMotor = ch_throttle + control_roll + control_pitch + control_yaw; // rear left motor
backMotor = ch_throttle - control_roll + control_pitch - control_yaw; // rear right motor
frontMotor = ch_throttle + control_roll + control_pitch - control_yaw; // front left motor
rightMotor = ch_throttle - control_roll + control_pitch + control_yaw; // front right motor
leftMotor = ch_throttle + control_roll - control_pitch + control_yaw; // rear left motor
backMotor = ch_throttle - control_roll - control_pitch - control_yaw; // rear right motor
#endif
}
if (motorArmed == 0) {