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ACM : Params - formatting cleanup

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This commit is contained in:
Jason Short 2012-09-10 20:22:11 -07:00
parent b787dc8cce
commit a73bc70553
1 changed files with 23 additions and 23 deletions
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46
ArduCopter/Parameters.h
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@ -358,53 +358,53 @@ public:
Parameters() : Parameters() :
#if FRAME_CONFIG == HELI_FRAME #if FRAME_CONFIG == HELI_FRAME
heli_servo_1 (CH_1), heli_servo_1 (CH_1),
heli_servo_2 (CH_2), heli_servo_2 (CH_2),
heli_servo_3 (CH_3), heli_servo_3 (CH_3),
heli_servo_4 (CH_4), heli_servo_4 (CH_4),
#endif #endif
rc_1 (CH_1), rc_1 (CH_1),
rc_2 (CH_2), rc_2 (CH_2),
rc_3 (CH_3), rc_3 (CH_3),
rc_4 (CH_4), rc_4 (CH_4),
rc_5 (CH_5), rc_5 (CH_5),
rc_6 (CH_6), rc_6 (CH_6),
rc_7 (CH_7), rc_7 (CH_7),
rc_8 (CH_8), rc_8 (CH_8),
#if MOUNT == ENABLED #if MOUNT == ENABLED
rc_10 (CH_10), rc_10 (CH_10),
rc_11 (CH_11), rc_11 (CH_11),
#endif #endif
// PID controller initial P initial I initial D // PID controller initial P initial I initial D
// initial imax // initial imax
//----------------------------------------------------------------------------------------------------- //-----------------------------------------------------------------------------------------------------
pid_rate_roll (RATE_ROLL_P, RATE_ROLL_I, RATE_ROLL_D, RATE_ROLL_IMAX * 100), pid_rate_roll (RATE_ROLL_P, RATE_ROLL_I, RATE_ROLL_D, RATE_ROLL_IMAX * 100),
pid_rate_pitch (RATE_PITCH_P, RATE_PITCH_I, RATE_PITCH_D, RATE_PITCH_IMAX * 100), pid_rate_pitch (RATE_PITCH_P, RATE_PITCH_I, RATE_PITCH_D, RATE_PITCH_IMAX * 100),
pid_rate_yaw (RATE_YAW_P, RATE_YAW_I, RATE_YAW_D, RATE_YAW_IMAX * 100), pid_rate_yaw (RATE_YAW_P, RATE_YAW_I, RATE_YAW_D, RATE_YAW_IMAX * 100),
pid_loiter_rate_lat (LOITER_RATE_P, LOITER_RATE_I, LOITER_RATE_D, LOITER_RATE_IMAX * 100), pid_loiter_rate_lat (LOITER_RATE_P, LOITER_RATE_I, LOITER_RATE_D, LOITER_RATE_IMAX * 100),
pid_loiter_rate_lon (LOITER_RATE_P, LOITER_RATE_I, LOITER_RATE_D, LOITER_RATE_IMAX * 100), pid_loiter_rate_lon (LOITER_RATE_P, LOITER_RATE_I, LOITER_RATE_D, LOITER_RATE_IMAX * 100),
pid_nav_lat (NAV_P, NAV_I, NAV_D, NAV_IMAX * 100), pid_nav_lat (NAV_P, NAV_I, NAV_D, NAV_IMAX * 100),
pid_nav_lon (NAV_P, NAV_I, NAV_D, NAV_IMAX * 100), pid_nav_lon (NAV_P, NAV_I, NAV_D, NAV_IMAX * 100),
pid_throttle (THROTTLE_P, THROTTLE_I, THROTTLE_D, THROTTLE_IMAX), pid_throttle (THROTTLE_P, THROTTLE_I, THROTTLE_D, THROTTLE_IMAX),
pid_optflow_roll (OPTFLOW_ROLL_P, OPTFLOW_ROLL_I, OPTFLOW_ROLL_D, OPTFLOW_IMAX * 100), pid_optflow_roll (OPTFLOW_ROLL_P, OPTFLOW_ROLL_I, OPTFLOW_ROLL_D, OPTFLOW_IMAX * 100),
pid_optflow_pitch (OPTFLOW_PITCH_P, OPTFLOW_PITCH_I, OPTFLOW_PITCH_D, OPTFLOW_IMAX * 100), pid_optflow_pitch (OPTFLOW_PITCH_P, OPTFLOW_PITCH_I, OPTFLOW_PITCH_D, OPTFLOW_IMAX * 100),
// PI controller initial P initial I initial // PI controller initial P initial I initial
// imax // imax
//---------------------------------------------------------------------- //----------------------------------------------------------------------
pi_loiter_lat (LOITER_P, LOITER_I, LOITER_IMAX * 100), pi_loiter_lat (LOITER_P, LOITER_I, LOITER_IMAX * 100),
pi_loiter_lon (LOITER_P, LOITER_I, LOITER_IMAX * 100), pi_loiter_lon (LOITER_P, LOITER_I, LOITER_IMAX * 100),
pi_stabilize_roll (STABILIZE_ROLL_P, STABILIZE_ROLL_I, STABILIZE_ROLL_IMAX * 100), pi_stabilize_roll (STABILIZE_ROLL_P, STABILIZE_ROLL_I, STABILIZE_ROLL_IMAX * 100),
pi_stabilize_pitch (STABILIZE_PITCH_P, STABILIZE_PITCH_I, STABILIZE_PITCH_IMAX * 100), pi_stabilize_pitch (STABILIZE_PITCH_P, STABILIZE_PITCH_I, STABILIZE_PITCH_IMAX * 100),
pi_stabilize_yaw (STABILIZE_YAW_P, STABILIZE_YAW_I, STABILIZE_YAW_IMAX * 100), pi_stabilize_yaw (STABILIZE_YAW_P, STABILIZE_YAW_I, STABILIZE_YAW_IMAX * 100),
pi_alt_hold (ALT_HOLD_P, ALT_HOLD_I, ALT_HOLD_IMAX) pi_alt_hold (ALT_HOLD_P, ALT_HOLD_I, ALT_HOLD_IMAX)
{ {
} }
}; };