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APM_Control: fixed some documentation (old parameter names)

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This commit is contained in:
Andrew Tridgell 2013-05-30 21:46:45 +10:00
parent 38e414db33
commit 53d3ce7d2c
1 changed files with 3 additions and 3 deletions
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6
libraries/APM_Control/AP_RollController.cpp
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@ -26,7 +26,7 @@ const AP_Param::GroupInfo AP_RollController::var_info[] PROGMEM = {
// @Param: K_P
// @DisplayName: Proportional Gain
// @Description: This is the gain from bank angle to aileron. This gain works the same way as the P term in the old PID (PTCH2SRV_P) and can be set to the same value.
// @Description: This is the gain from bank angle to aileron. This gain works the same way as the P term in the old PID (RLL2SRV_P) and can be set to the same value.
// @Range: 0.1 1.0
// @Increment: 0.1
// @User: User
@ -34,7 +34,7 @@ const AP_Param::GroupInfo AP_RollController::var_info[] PROGMEM = {
// @Param: K_D
// @DisplayName: Damping Gain
// @Description: This is the gain from roll rate to aileron. This adjusts the damping of the roll control loop. It has the same effect as PTCH2SRV_D in the old PID controller but without the spikes in servo demands. This gain helps to reduce rolling in turbulence. It should be increased in 0.01 increments as too high a value can lead to a high frequency pitch oscillation that could overstress the airframe.
// @Description: This is the gain from roll rate to aileron. This adjusts the damping of the roll control loop. It has the same effect as RLL2SRV_D in the old PID controller but without the spikes in servo demands. This gain helps to reduce rolling in turbulence. It should be increased in 0.01 increments as too high a value can lead to a high frequency pitch oscillation that could overstress the airframe.
// @Range: 0 0.1
// @Increment: 0.01
// @User: User
@ -42,7 +42,7 @@ const AP_Param::GroupInfo AP_RollController::var_info[] PROGMEM = {
// @Param: K_I
// @DisplayName: Integrator Gain
// @Description: This is the gain from the integral of bank angle to aileron. It has the same effect as PTCH2SRV_I in the old PID controller. Increasing this gain causes the controller to trim out steady offsets due to an out of trim aircraft.
// @Description: This is the gain from the integral of bank angle to aileron. It has the same effect as RLL2SRV_I in the old PID controller. Increasing this gain causes the controller to trim out steady offsets due to an out of trim aircraft.
// @Range: 0 1.0
// @Increment: 0.05
// @User: User