AP_NavEKF3: Update param descriptions

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Paul Riseborough 2020-11-22 10:48:37 +11:00 committed by Andrew Tridgell
parent 4f4a2f446d
commit ab05e8ed4a

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@ -193,17 +193,14 @@ const AP_Param::GroupInfo NavEKF3::var_info[] = {
// @Param: BCOEF_X // @Param: BCOEF_X
// @DisplayName: Ballistic coefficient measured in X direction // @DisplayName: Ballistic coefficient measured in X direction
// @Description: Ratio of mass to drag coefficient measured along the X body axis. This parameter enables estimation of wind drift for vehicles with bluff bodies and without propulsion forces in the X and Y direction (eg multicopters). The drag produced by this effect scales with speed squared. Set to a postive value > 1.0 to enable. A starting value is the mass in Kg divided by the frontal area. The predicted drag from the rotors is specified separately by the EK3_MCOEF parameter. // @Description: Ratio of mass to drag coefficient measured along the X body axis. This parameter enables estimation of wind drift for vehicles with bluff bodies and without propulsion forces in the X and Y direction (eg multicopters). The drag produced by this effect scales with speed squared. Set to a postive value > 1.0 to enable. A starting value is the mass in Kg divided by the frontal area. The predicted drag from the rotors is specified separately by the EK3_MCOEF parameter.
// @Range: 0.0 100.0 // @Range: 0.0 1000.0
// @Increment: 1.0
// @User: Advanced // @User: Advanced
// @Param: BCOEF_Y // @Param: BCOEF_Y
// @DisplayName: Ballistic coefficient measured in Y direction // @DisplayName: Ballistic coefficient measured in Y direction
// @Description: Ratio of mass to drag coefficient measured along the Y body axis. This parameter enables estimation of wind drift for vehicles with bluff bodies and without propulsion forces in the X and Y direction (eg multicopters). The drag produced by this effect scales with speed squared. Set to a postive value > 1.0 to enable. A starting value is the mass in Kg divided by the side area. The predicted drag from the rotors is specified separately by the EK3_MCOEF parameter. // @Description: Ratio of mass to drag coefficient measured along the Y body axis. This parameter enables estimation of wind drift for vehicles with bluff bodies and without propulsion forces in the X and Y direction (eg multicopters). The drag produced by this effect scales with speed squared. Set to a postive value > 1.0 to enable. A starting value is the mass in Kg divided by the side area. The predicted drag from the rotors is specified separately by the EK3_MCOEF parameter.
// @Range: 50.0 1000.0 // @Range: 50.0 1000.0
// @Increment: 10.0
// @User: Advanced // @User: Advanced
// @Param: BCOEF_Y
// @Param: BCOEF_Z // @Param: BCOEF_Z
// @DisplayName: unused // @DisplayName: unused