|
def | pymavlink.mavextra.airspeed (VFR_HUD, ratio=None, used_ratio=None, offset=None) |
|
def | pymavlink.mavextra.airspeed_energy_error (NAV_CONTROLLER_OUTPUT, VFR_HUD) |
|
def | pymavlink.mavextra.airspeed_ratio (VFR_HUD) |
|
def | pymavlink.mavextra.airspeed_voltage (VFR_HUD, ratio=None) |
|
def | pymavlink.mavextra.altitude (SCALED_PRESSURE, ground_pressure=None, ground_temp=None) |
|
def | pymavlink.mavextra.altitude2 (SCALED_PRESSURE, ground_pressure=None, ground_temp=None) |
|
def | pymavlink.mavextra.angle_diff (angle1, angle2) |
|
def | pymavlink.mavextra.armed (HEARTBEAT) |
|
def | pymavlink.mavextra.average (var, key, N) |
|
def | pymavlink.mavextra.DCM_update (IMU, ATT, MAG, GPS) |
|
def | pymavlink.mavextra.delta (var, key, tusec=None) |
|
def | pymavlink.mavextra.delta_angle (var, key, tusec=None) |
|
def | pymavlink.mavextra.demix1 (servo1, servo2, gain=0.5) |
|
def | pymavlink.mavextra.demix2 (servo1, servo2, gain=0.5) |
|
def | pymavlink.mavextra.diff (var, key) |
|
def | pymavlink.mavextra.distance_gps2 (GPS, GPS2) |
|
def | pymavlink.mavextra.distance_home (GPS_RAW) |
|
def | pymavlink.mavextra.distance_two (GPS_RAW1, GPS_RAW2, horizontal=True) |
|
def | pymavlink.mavextra.downsample (N) |
|
def | pymavlink.mavextra.earth_accel (RAW_IMU, ATTITUDE) |
|
def | pymavlink.mavextra.earth_accel2 (RAW_IMU, ATTITUDE) |
|
def | pymavlink.mavextra.earth_accel2_df (IMU, IMU2, ATT) |
|
def | pymavlink.mavextra.earth_accel_df (IMU, ATT) |
|
def | pymavlink.mavextra.earth_gyro (RAW_IMU, ATTITUDE) |
|
def | pymavlink.mavextra.earth_rates (ATTITUDE) |
|
def | pymavlink.mavextra.EAS2TAS (ARSP, GPS, BARO, ground_temp=25) |
|
def | pymavlink.mavextra.ekf1_pos (EKF1) |
|
def | pymavlink.mavextra.energy_error (NAV_CONTROLLER_OUTPUT, VFR_HUD) |
|
def | pymavlink.mavextra.euler_p90 (MSG) |
|
def | pymavlink.mavextra.euler_rotated (MSG, roll, pitch, yaw) |
|
def | pymavlink.mavextra.euler_to_quat (e) |
|
def | pymavlink.mavextra.expected_mag (RAW_IMU, ATTITUDE, inclination, declination) |
|
def | pymavlink.mavextra.expected_magx (RAW_IMU, ATTITUDE, inclination, declination) |
|
def | pymavlink.mavextra.expected_magy (RAW_IMU, ATTITUDE, inclination, declination) |
|
def | pymavlink.mavextra.expected_magz (RAW_IMU, ATTITUDE, inclination, declination) |
|
def | pymavlink.mavextra.get_motor_offsets (SERVO_OUTPUT_RAW, ofs, motor_ofs) |
|
def | pymavlink.mavextra.gps_newpos (lat, lon, bearing, distance) |
|
def | pymavlink.mavextra.gps_offset (lat, lon, east, north) |
|
def | pymavlink.mavextra.gps_velocity (GLOBAL_POSITION_INT) |
|
def | pymavlink.mavextra.gps_velocity_body (GPS_RAW_INT, ATTITUDE) |
|
def | pymavlink.mavextra.gps_velocity_df (GPS) |
|
def | pymavlink.mavextra.gps_velocity_old (GPS_RAW_INT) |
|
def | pymavlink.mavextra.gravity (RAW_IMU, SENSOR_OFFSETS=None, ofs=None, mul=None, smooth=0.7) |
|
def | pymavlink.mavextra.kmh (mps) |
|
def | pymavlink.mavextra.lowpass (var, key, factor) |
|
def | pymavlink.mavextra.mag_discrepancy (RAW_IMU, ATTITUDE, inclination, declination=None) |
|
def | pymavlink.mavextra.mag_field (RAW_IMU, SENSOR_OFFSETS=None, ofs=None) |
|
def | pymavlink.mavextra.mag_field_df (MAG, ofs=None) |
|
def | pymavlink.mavextra.mag_field_motors (RAW_IMU, SENSOR_OFFSETS, ofs, SERVO_OUTPUT_RAW, motor_ofs) |
|
def | pymavlink.mavextra.mag_heading (RAW_IMU, ATTITUDE, declination=None, SENSOR_OFFSETS=None, ofs=None) |
|
def | pymavlink.mavextra.mag_heading_motors (RAW_IMU, ATTITUDE, declination, SENSOR_OFFSETS, ofs, SERVO_OUTPUT_RAW, motor_ofs) |
|
def | pymavlink.mavextra.mag_inclination (RAW_IMU, ATTITUDE, declination=None) |
|
def | pymavlink.mavextra.mag_pitch (RAW_IMU, inclination, declination) |
|
def | pymavlink.mavextra.mag_roll (RAW_IMU, inclination, declination) |
|
def | pymavlink.mavextra.mag_rotation (RAW_IMU, inclination, declination) |
|
def | pymavlink.mavextra.mag_yaw (RAW_IMU, inclination, declination) |
|
def | pymavlink.mavextra.mix1 (servo1, servo2, mixtype=1, gain=0.5) |
|
def | pymavlink.mavextra.mix2 (servo1, servo2, mixtype=1, gain=0.5) |
|
def | pymavlink.mavextra.mixer (servo1, servo2, mixtype=1, gain=0.5) |
|
def | pymavlink.mavextra.pitch_estimate (RAW_IMU, GPS_RAW_INT=None, ATTITUDE=None, SENSOR_OFFSETS=None, ofs=None, mul=None, smooth=0.7) |
|
def | pymavlink.mavextra.pitch_rate (ATTITUDE) |
|
def | pymavlink.mavextra.pitch_sim (SIMSTATE, GPS_RAW) |
|
def | pymavlink.mavextra.PX4_update (IMU, ATT) |
|
def | pymavlink.mavextra.qpitch (MSG) |
|
def | pymavlink.mavextra.qpitch_p90 (MSG) |
|
def | pymavlink.mavextra.qroll (MSG) |
|
def | pymavlink.mavextra.qroll_p90 (MSG) |
|
def | pymavlink.mavextra.quat_to_euler (q) |
|
def | pymavlink.mavextra.qyaw (MSG) |
|
def | pymavlink.mavextra.qyaw_p90 (MSG) |
|
def | pymavlink.mavextra.rate_of_turn (speed, bank) |
|
def | pymavlink.mavextra.roll_estimate (RAW_IMU, GPS_RAW_INT=None, ATTITUDE=None, SENSOR_OFFSETS=None, ofs=None, mul=None, smooth=0.7) |
|
def | pymavlink.mavextra.roll_rate (ATTITUDE) |
|
def | pymavlink.mavextra.rotate_quat (attitude, roll, pitch, yaw) |
|
def | pymavlink.mavextra.rotation (ATTITUDE) |
|
def | pymavlink.mavextra.rotation2 (AHRS2) |
|
def | pymavlink.mavextra.rotation_df (ATT) |
|
def | pymavlink.mavextra.rover_lat_accel (VFR_HUD, SERVO_OUTPUT_RAW) |
|
def | pymavlink.mavextra.rover_turn_circle (SERVO_OUTPUT_RAW) |
|
def | pymavlink.mavextra.rover_yaw_rate (VFR_HUD, SERVO_OUTPUT_RAW) |
|
def | pymavlink.mavextra.sawtooth (ATTITUDE, amplitude=2.0, period=5.0) |
|
def | pymavlink.mavextra.second_derivative_5 (var, key) |
|
def | pymavlink.mavextra.second_derivative_9 (var, key) |
|
def | pymavlink.mavextra.wingloading (bank) |
|
def | pymavlink.mavextra.wrap_180 (angle) |
|
def | pymavlink.mavextra.wrap_360 (angle) |
|
def | pymavlink.mavextra.wrap_valid_longitude (lon) |
|
def | pymavlink.mavextra.yaw_rate (ATTITUDE) |
|