ardupilot/ArduCopter/drift.pde

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////////////////////////////////////////////////////////////////////////////////
// Drift Mode
////////////////////////////////////////////////////////////////////////////////
#define SPEEDGAIN 14.0
// The function call for managing the flight mode drift
static void
get_roll_pitch_drift()
{
}
static void
get_yaw_drift()
{
static float breaker = 0.0;
// convert pilot input to lean angles
// moved to Yaw since it is called before get_roll_pitch_drift();
get_pilot_desired_lean_angles(g.rc_1.control_in, g.rc_2.control_in, control_roll, control_pitch);
// Grab inertial velocity
Vector3f vel = inertial_nav.get_velocity();
// rotate roll, pitch input from north facing to vehicle's perspective
float roll_vel = vel.y * cos_yaw - vel.x * sin_yaw; // body roll vel
float pitch_vel = vel.y * sin_yaw + vel.x * cos_yaw; // body pitch vel
float pitch_vel2 = min(fabs(pitch_vel), 800);
// simple gain scheduling for yaw input
get_yaw_rate_stabilized_ef((float)(control_roll/2) * (1.0 - (pitch_vel2 / 2400.0)));
roll_vel = constrain_float(roll_vel, -322, 322);
pitch_vel = constrain_float(pitch_vel, -322, 322);
// always limit roll
get_stabilize_roll(roll_vel * -SPEEDGAIN);
if(control_pitch == 0){
// .14/ (.03 * 100) = 4.6 seconds till full breaking
breaker+= .03;
breaker = min(breaker, SPEEDGAIN);
// If we let go of sticks, bring us to a stop
get_stabilize_pitch(pitch_vel * breaker);
}else{
breaker = 0.0;
get_stabilize_pitch(control_pitch);
}
}