| All good, valid response + data |
200 |
|
| int16_t |
_servo1_pos |
Angular location of swash servo #1 |
| int16_t |
_servo2_pos |
Angular location of swash servo #2 |
| int16_t |
_servo3_pos |
Angular location of swash servo #3 |
| int16_t |
_servo4_pos |
Angular location of swash servo #4 |
| int16_t |
_roll_max |
Maximum roll angle of the swash plate in centi-degrees |
| int16_t |
_pitch_max |
Maximum pitch angle of the swash plate in centi-degrees |
| int16_t |
_collective_min |
Lowest possible servo position for the swashplate |
| int16_t |
_collective_max |
Highest possible servo position for the swashplate |
| int16_t |
_collective_mid |
Swash servo position corresponding to zero collective pitch (or zero lift for Assymetrical blades) |
| int16_t |
_collective_upper_trim_min |
Lowest possible servo4 position for upper rotor pitch trim |
| int16_t |
_collective_upper_trim_max |
Highest possible servo4 position for upper rotor pitch trim |
| int8_t |
_servo_manual |
Pass radio inputs directly to servos during set-up through mission planner |
| int16_t |
_phase_angle |
Phase angle correction for rotor head. If pitching the swash forward induces a roll, this can be correct the problem |
| int16_t |
_collective_yaw_effect |
Feed-forward compensation to automatically add rudder input when collective pitch is increased. Can be positive or negative depending on mechanics. |
| int8_t |
_rsc_ramp_time |
Time in seconds for the output to the main rotor's ESC to reach full speed |
| int8_t |
_rsc_runup_time |
Time in seconds for the main rotor to reach full speed. Must be longer than _rsc_ramp_time |
| int8_t |
_tail_ramp_time |
Time in seconds for the output to the main rotor's ESC to reach full speed |
| int16_t |
_land_collective_min |
Minimum collective when landed or landing |
| float |
_rollFactor[4] |
Roll factor of each servo for calculating roll output of rotors |
| float |
_pitchFactor[4] |
Pitch factor of each servo for calculating pitch output of rotors |
| float |
_collectiveFactor[4] |
Collective Pitch factor of each servo for rotors |
| float |
_collectiveFactorUpper[4] |
Collective Pitch factor of each servo for upper rotor |
| float |
_roll_scaler |
scaler to convert roll input from radio (i.e. -4500 ~ 4500) to max roll range |
| float |
_pitch_scaler |
scaler to convert pitch input from radio (i.e. -4500 ~ 4500) to max pitch range |
| float |
_collective_scalar |
collective scalar to convert pwm form (i.e. 0 ~ 1000) passed in to actual servo range (i.e 1250~1750 would be 500) |
| float |
_collective_scalar_manual |
collective scalar to reduce the range of the collective movement while collective is being controlled manually (i.e. directly by the pilot) |
| int16_t |
_collective_out |
actual collective pitch value. Required by the main code for calculating cruise throttle |
| int16_t |
_collective_mid_pwm |
collective mid parameter value converted to pwm form (i.e. 0 ~ 1000) |
| int16_t |
_rotor_desired |
latest desired rotor speed from pilot |
| float |
_rotor_out |
latest output sent to the main rotor or an estimate of the rotors actual speed (whichever is higher) (0 ~ 1000) |
| float |
_rsc_ramp_increment |
the amount we can increase the rotor output during each iteration |
| float |
_rsc_runup_increment |
the amount we can increase the rotor's estimated speed during each iteration |
| float |
_rotor_speed_estimate |
estimated speed of the main rotor (0~1000) |
| float |
_tail_ramp_increment |
the amount we can increase the rotor output during each iteration |
| float |
_tail_out |
latest output sent to the main rotor or an estimate of the rotors actual speed (whichever is higher) (0 ~ 1000) |
| Invalid API end-point (bad url) |
404 |
|
| Invalid Arguments in the POST body |
400 |
|
| Invalid content-type |
415 |
|
| Unsupported media type |
415 |
|
Invalid API version (through Accept header) |
406 |
|
| Backend error (backend API down, etc) |
500 |
|