Specifies the most gradient with the terrain underneath the automobile when it is actually working with variety finder like a peak reference
Z position of the main IMU accelerometer in physique body. Optimistic Z is down through the origin. Focus: The IMU really should be located as close to the motor vehicle c.g. as simple in order that the worth of this parameter is minimised.
Time in milliseconds that the rangefinder reading can take to settle. This is certainly only made use of every time a STOP_PIN is specified. It determines just how long we need to wait for the rangefinder to present a reading through after we set the STOP_PIN significant.
Electronic pin that enables/disables rangefinder measurement for an analog rangefinder. A worth of -1 indicates no pin.
Perform assigned to this servo. Looking at this to Disabled(0) will setup this output for Manage by vehicle missions or MAVLink servo set instructions. another benefit will permit the corresponding function
This is the volume of msec the optical circulation measurements lag driving the inertial measurements. It's the time with the stop with the optical flow averaging interval and isn't going to incorporate enough time delay because of the 100msec of averaging throughout the circulation sensor.
This state method sounds controls The expansion of system magnetic field state error estimates. Escalating it helps make magnetometer bias error estimation quicker and noisier.
Compensates for that pitch angle distinction between the control board and also the frame. Positive values make the vehicle pitch up/again.
The volume of mission mission items which has been loaded by the ground station. Usually do not modify this manually.
This sets The proportion variety of standard deviations applied to the GPS velocity measurement innovation regularity check. Lowering it causes it to be a lot more probable that superior measurements willbe rejected. Escalating it makes it more most likely that undesirable measurements might be acknowledged.
This allows EKF2. Enabling EKF2 only tends to make the maths operate, it does not suggest it will be employed for flight Manage. To make use of it for flight Command established AHRS_EKF_TYPE=2. A reboot or restart will need to be performed click here after altering the value of EK2_ENABLE for it to acquire influence.
This sets The share selection of standard deviations applied to the GPS placement measurement innovation consistency check. Reducing it causes it to be more likely that very good measurements are going to be turned down. Increasing it makes it additional probable that lousy measurements will be accepted.
This controls the amount the procedure sound around the wind states is elevated when attaining or shedding altitude to take into account changes in wind pace and path with altitude.
Y posture of the main rangefinder in physique body. Optimistic Y is to the right of your origin. Make use of the zero vary datum place if supplied.