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Copter: STB_RLL_P and STB_PIT_P @Range 3 to 12

This commit is contained in:
Randy Mackay 2014-04-21 10:41:01 +09:00
parent 41100a13c3
commit a1edf347bf
1 changed files with 2 additions and 2 deletions
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4
ArduCopter/Parameters.pde
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@ -801,7 +801,7 @@ const AP_Param::Info var_info[] PROGMEM = {
// @Param: STB_RLL_P // @Param: STB_RLL_P
// @DisplayName: Roll axis stabilize controller P gain // @DisplayName: Roll axis stabilize controller P gain
// @Description: Roll axis stabilize (i.e. angle) controller P gain. Converts the error between the desired roll angle and actual angle to a desired roll rate // @Description: Roll axis stabilize (i.e. angle) controller P gain. Converts the error between the desired roll angle and actual angle to a desired roll rate
// @Range: 3.000 6.000 // @Range: 3.000 12.000
// @User: Standard // @User: Standard
// @Param: STB_RLL_I // @Param: STB_RLL_I
@ -821,7 +821,7 @@ const AP_Param::Info var_info[] PROGMEM = {
// @Param: STB_PIT_P // @Param: STB_PIT_P
// @DisplayName: Pitch axis stabilize controller P gain // @DisplayName: Pitch axis stabilize controller P gain
// @Description: Pitch axis stabilize (i.e. angle) controller P gain. Converts the error between the desired pitch angle and actual angle to a desired pitch rate // @Description: Pitch axis stabilize (i.e. angle) controller P gain. Converts the error between the desired pitch angle and actual angle to a desired pitch rate
// @Range: 3.000 6.000 // @Range: 3.000 12.000
// @User: Standard // @User: Standard
GGROUP(p_stabilize_pitch, "STB_PIT_", AC_P), GGROUP(p_stabilize_pitch, "STB_PIT_", AC_P),