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AP_NavEKF3: Update param descriptions
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@ -193,17 +193,14 @@ const AP_Param::GroupInfo NavEKF3::var_info[] = {
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// @Param: BCOEF_X
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// @Param: BCOEF_X
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// @DisplayName: Ballistic coefficient measured in X direction
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// @DisplayName: Ballistic coefficient measured in X direction
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// @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.
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// @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.
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// @Range: 0.0 100.0
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// @Range: 0.0 1000.0
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// @Increment: 1.0
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// @User: Advanced
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// @User: Advanced
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// @Param: BCOEF_Y
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// @Param: BCOEF_Y
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// @DisplayName: Ballistic coefficient measured in Y direction
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// @DisplayName: Ballistic coefficient measured in Y direction
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// @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.
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// @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.
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// @Range: 50.0 1000.0
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// @Range: 50.0 1000.0
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// @Increment: 10.0
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// @User: Advanced
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// @User: Advanced
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// @Param: BCOEF_Y
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// @Param: BCOEF_Z
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// @Param: BCOEF_Z
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// @DisplayName: unused
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// @DisplayName: unused
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