aepko/Ardupilot2
1
0
Fork 0
Code Issues Pull Requests Actions Packages Projects Releases Wiki Activity

SITL: reformat SITL code with astyle

Browse Source
This commit is contained in:
Andrew Tridgell 2015-05-05 11:49:54 +10:00
parent c81ad1d622
commit 42c6801d61
10 changed files with 122 additions and 117 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

6
libraries/SITL/SIM_Aircraft.cpp
View File

@ -233,9 +233,9 @@ void Aircraft::fill_fdm(struct sitl_fdm &fdm) const
uint64_t Aircraft::get_wall_time_us() const
{
struct timeval tp;
gettimeofday(&tp,NULL);
return tp.tv_sec*1.0e6 + tp.tv_usec;
struct timeval tp;
gettimeofday(&tp,NULL);
return tp.tv_sec*1.0e6 + tp.tv_usec;
}
/*

4
libraries/SITL/SIM_Helicopter.h
View File

@ -34,7 +34,9 @@ public:
void update(const struct sitl_input &input);
/* static object creator */
static Aircraft *create(const char *home_str, const char *frame_str) { return new Helicopter(home_str, frame_str); }
static Aircraft *create(const char *home_str, const char *frame_str) {
return new Helicopter(home_str, frame_str);
}
private:
float terminal_rotation_rate;

6
libraries/SITL/SIM_Multicopter.h
View File

@ -35,7 +35,7 @@ public:
angle(_angle), // angle in degrees from front
clockwise(_clockwise), // clockwise == true, anti-clockwise == false
servo(_servo) // what servo output drives this motor
{}
{}
};
/*
@ -67,7 +67,9 @@ public:
void update(const struct sitl_input &input);
/* static object creator */
static Aircraft *create(const char *home_str, const char *frame_str) { return new MultiCopter(home_str, frame_str); }
static Aircraft *create(const char *home_str, const char *frame_str) {
return new MultiCopter(home_str, frame_str);
}
private:
const Frame *frame;

4
libraries/SITL/SIM_Rover.h
View File

@ -34,7 +34,9 @@ public:
void update(const struct sitl_input &input);
/* static object creator */
static Aircraft *create(const char *home_str, const char *frame_str) { return new Rover(home_str, frame_str); }
static Aircraft *create(const char *home_str, const char *frame_str) {
return new Rover(home_str, frame_str);
}
private:
float max_speed;

73
libraries/SITL/SITL.cpp
View File

@ -15,8 +15,7 @@
*/
/*
SITL.cpp - software in the loop state
SITL.cpp - software in the loop state
*/
#include <AP_Common.h>
@ -77,20 +76,20 @@ const AP_Param::GroupInfo SITL::var_info[] PROGMEM = {
/* report SITL state via MAVLink */
void SITL::simstate_send(mavlink_channel_t chan)
{
double p, q, r;
float yaw;
double p, q, r;
float yaw;
// we want the gyro values to be directly comparable to the
// raw_imu message, which is in body frame
convert_body_frame(state.rollDeg, state.pitchDeg,
// we want the gyro values to be directly comparable to the
// raw_imu message, which is in body frame
convert_body_frame(state.rollDeg, state.pitchDeg,
state.rollRate, state.pitchRate, state.yawRate,
&p, &q, &r);
// convert to same conventions as DCM
yaw = state.yawDeg;
if (yaw > 180) {
yaw -= 360;
}
// convert to same conventions as DCM
yaw = state.yawDeg;
if (yaw > 180) {
yaw -= 360;
}
mavlink_msg_simstate_send(chan,
ToRad(state.rollDeg),
@ -107,30 +106,30 @@ void SITL::simstate_send(mavlink_channel_t chan)
/* report SITL state to DataFlash */
void SITL::Log_Write_SIMSTATE(DataFlash_Class &DataFlash)
{
double p, q, r;
float yaw;
double p, q, r;
float yaw;
// we want the gyro values to be directly comparable to the
// raw_imu message, which is in body frame
convert_body_frame(state.rollDeg, state.pitchDeg,
// we want the gyro values to be directly comparable to the
// raw_imu message, which is in body frame
convert_body_frame(state.rollDeg, state.pitchDeg,
state.rollRate, state.pitchRate, state.yawRate,
&p, &q, &r);
// convert to same conventions as DCM
yaw = state.yawDeg;
if (yaw > 180) {
yaw -= 360;
}
// convert to same conventions as DCM
yaw = state.yawDeg;
if (yaw > 180) {
yaw -= 360;
}
struct log_AHRS pkt = {
LOG_PACKET_HEADER_INIT(LOG_SIMSTATE_MSG),
time_ms : hal.scheduler->millis(),
roll : (int16_t)(state.rollDeg*100),
pitch : (int16_t)(state.pitchDeg*100),
yaw : (uint16_t)(wrap_360_cd(yaw*100)),
alt : (float)state.altitude,
lat : (int32_t)(state.latitude*1.0e7),
lng : (int32_t)(state.longitude*1.0e7)
roll : (int16_t)(state.rollDeg*100),
pitch : (int16_t)(state.pitchDeg*100),
yaw : (uint16_t)(wrap_360_cd(yaw*100)),
alt : (float)state.altitude,
lat : (int32_t)(state.latitude*1.0e7),
lng : (int32_t)(state.longitude*1.0e7)
};
DataFlash.WriteBlock(&pkt, sizeof(pkt));
}
@ -143,17 +142,17 @@ void SITL::convert_body_frame(double rollDeg, double pitchDeg,
double rollRate, double pitchRate, double yawRate,
double *p, double *q, double *r)
{
double phi, theta, phiDot, thetaDot, psiDot;
double phi, theta, phiDot, thetaDot, psiDot;
phi = ToRad(rollDeg);
theta = ToRad(pitchDeg);
phiDot = ToRad(rollRate);
thetaDot = ToRad(pitchRate);
psiDot = ToRad(yawRate);
phi = ToRad(rollDeg);
theta = ToRad(pitchDeg);
phiDot = ToRad(rollRate);
thetaDot = ToRad(pitchRate);
psiDot = ToRad(yawRate);
*p = phiDot - psiDot*sinf(theta);
*q = cosf(phi)*thetaDot + sinf(phi)*psiDot*cosf(theta);
*r = cosf(phi)*psiDot*cosf(theta) - sinf(phi)*thetaDot;
*p = phiDot - psiDot*sinf(theta);
*q = cosf(phi)*thetaDot + sinf(phi)*psiDot*cosf(theta);
*r = cosf(phi)*psiDot*cosf(theta) - sinf(phi)*thetaDot;
}

86
libraries/SITL/SITL.h
View File

@ -10,19 +10,19 @@
#include <DataFlash.h>
struct PACKED sitl_fdm {
// this is the packet sent by the simulator
// to the APM executable to update the simulator state
// All values are little-endian
// this is the packet sent by the simulator
// to the APM executable to update the simulator state
// All values are little-endian
uint64_t timestamp_us;
double latitude, longitude; // degrees
double altitude; // MSL
double heading; // degrees
double speedN, speedE, speedD; // m/s
double xAccel, yAccel, zAccel; // m/s/s in body frame
double rollRate, pitchRate, yawRate; // degrees/s/s in earth frame
double rollDeg, pitchDeg, yawDeg; // euler angles, degrees
double airspeed; // m/s
uint32_t magic; // 0x4c56414f
double latitude, longitude; // degrees
double altitude; // MSL
double heading; // degrees
double speedN, speedE, speedD; // m/s
double xAccel, yAccel, zAccel; // m/s/s in body frame
double rollRate, pitchRate, yawRate; // degrees/s/s in earth frame
double rollDeg, pitchDeg, yawDeg; // euler angles, degrees
double airspeed; // m/s
uint32_t magic; // 0x4c56414f
};
@ -46,34 +46,34 @@ public:
GPS_TYPE_SBP = 6,
};
struct sitl_fdm state;
struct sitl_fdm state;
static const struct AP_Param::GroupInfo var_info[];
static const struct AP_Param::GroupInfo var_info[];
// noise levels for simulated sensors
AP_Float baro_noise; // in metres
AP_Float baro_drift; // in metres per second
AP_Float baro_glitch; // glitch in meters
AP_Float gyro_noise; // in degrees/second
AP_Float accel_noise; // in m/s/s
AP_Vector3f accel_bias; // in m/s/s
AP_Float aspd_noise; // in m/s
AP_Float mag_noise; // in mag units (earth field is 818)
AP_Float mag_error; // in degrees
AP_Vector3f mag_mot; // in mag units per amp
AP_Vector3f mag_ofs; // in mag units
// noise levels for simulated sensors
AP_Float baro_noise; // in metres
AP_Float baro_drift; // in metres per second
AP_Float baro_glitch; // glitch in meters
AP_Float gyro_noise; // in degrees/second
AP_Float accel_noise; // in m/s/s
AP_Vector3f accel_bias; // in m/s/s
AP_Float aspd_noise; // in m/s
AP_Float mag_noise; // in mag units (earth field is 818)
AP_Float mag_error; // in degrees
AP_Vector3f mag_mot; // in mag units per amp
AP_Vector3f mag_ofs; // in mag units
AP_Float servo_rate; // servo speed in degrees/second
AP_Float sonar_glitch;// probablility between 0-1 that any given sonar sample will read as max distance
AP_Float sonar_noise; // in metres
AP_Float sonar_scale; // meters per volt
AP_Float drift_speed; // degrees/second/minute
AP_Float drift_time; // period in minutes
AP_Float drift_speed; // degrees/second/minute
AP_Float drift_time; // period in minutes
AP_Float engine_mul; // engine multiplier
AP_Int8 gps_disable; // disable simulated GPS
AP_Int8 gps2_enable; // enable 2nd simulated GPS
AP_Int8 gps_delay; // delay in samples
AP_Int8 gps_disable; // disable simulated GPS
AP_Int8 gps2_enable; // enable 2nd simulated GPS
AP_Int8 gps_delay; // delay in samples
AP_Int8 gps_type; // see enum GPSType
AP_Float gps_byteloss;// byte loss as a percent
AP_Int8 gps_numsats; // number of visible satellites
@ -81,13 +81,13 @@ public:
AP_Int8 gps_hertz; // GPS update rate in Hz
AP_Float batt_voltage; // battery voltage base
AP_Float accel_fail; // accelerometer failure value
AP_Int8 rc_fail; // fail RC input
AP_Int8 baro_disable; // disable simulated barometer
AP_Int8 rc_fail; // fail RC input
AP_Int8 baro_disable; // disable simulated barometer
AP_Int8 float_exception; // enable floating point exception checks
AP_Int8 flow_enable; // enable simulated optflow
AP_Int16 flow_rate; // optflow data rate (Hz)
AP_Int8 flow_delay; // optflow data delay
AP_Int8 terrain_enable; // enable using terrain for height
AP_Int8 flow_enable; // enable simulated optflow
AP_Int16 flow_rate; // optflow data rate (Hz)
AP_Int8 flow_delay; // optflow data delay
AP_Int8 terrain_enable; // enable using terrain for height
// wind control
AP_Float wind_speed;
@ -99,16 +99,16 @@ public:
AP_Int16 mag_delay; // magnetometer data delay in ms
AP_Int16 wind_delay; // windspeed data delay in ms
void simstate_send(mavlink_channel_t chan);
void simstate_send(mavlink_channel_t chan);
void Log_Write_SIMSTATE(DataFlash_Class &dataflash);
// convert a set of roll rates from earth frame to body frame
static void convert_body_frame(double rollDeg, double pitchDeg,
double rollRate, double pitchRate, double yawRate,
double *p, double *q, double *r);
// convert a set of roll rates from earth frame to body frame
static void convert_body_frame(double rollDeg, double pitchDeg,
double rollRate, double pitchRate, double yawRate,
double *p, double *q, double *r);
// convert a set of roll rates from body frame to earth frame
// convert a set of roll rates from body frame to earth frame
static Vector3f convert_earth_frame(const Matrix3f &dcm, const Vector3f &gyro);
};