Mirror
/
ardupilot
mirror of https://github.com/ArduPilot/ardupilot
5
0
Fork 0
Code Issues Packages Projects Releases Wiki Activity

AP_Motors: example sketch can test helicopter

This commit is contained in:
Randy Mackay 2016-02-03 09:51:26 +09:00
parent 47873c1d34
commit 93597d152f
1 changed files with 25 additions and 9 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

34
libraries/AP_Motors/examples/AP_Motors_test/AP_Motors_test.cpp
View File

@ -40,7 +40,11 @@ void motor_order_test();
void stability_test();
void update_motors();
#define HELI_TEST 1 // set to 1 to test helicopters
#define NUM_OUTPUTS 4 // set to 6 for hexacopter, 8 for octacopter and heli
RC_Channel rc1(0), rc2(1), rc3(2), rc4(3);
RC_Channel rc7(6), rsc(8), h1(0), h2(1), h3(2), h4(3);
// uncomment the row below depending upon what frame you are using
//AP_MotorsTri motors(400);
@ -49,8 +53,7 @@ AP_MotorsQuad motors(400);
//AP_MotorsY6 motors(400);
//AP_MotorsOcta motors(400);
//AP_MotorsOctaQuad motors(400);
//AP_MotorsHeli motors(rc1, rc2, rc3, rc4, 400);
//AP_MotorsHeli_Single motors(rc7, rsc, h1, h2, h3, h4, 400);
// setup
void setup()
@ -61,8 +64,10 @@ void setup()
motors.set_update_rate(490);
motors.set_frame_orientation(AP_MOTORS_X_FRAME);
motors.Init();
#if HELI_TEST == 0
motors.set_throttle_range(130,1000,2000);
motors.set_hover_throttle(500);
#endif
motors.enable();
motors.output_min();
@ -136,6 +141,7 @@ void stability_test()
// arm motors
motors.armed(true);
motors.set_interlock(true);
//hal.console->printf("Roll,Pitch,Yaw,Thr,Mot1,Mot2,Mot3,Mot4,AvgOut\n"); // quad
//hal.console->printf("Roll,Pitch,Yaw,Thr,Mot1,Mot2,Mot3,Mot4,Mot5,Mot6,AvgOut\n"); // hexa
@ -155,13 +161,19 @@ void stability_test()
motors.set_yaw(yaw_in);
motors.set_throttle(throttle_in);
motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_THROTTLE_UNLIMITED);
#if HELI_TEST == 0
motors.set_throttle_mix_mid();
#endif
update_motors();
avg_out = ((hal.rcout->read(0) + hal.rcout->read(1) + hal.rcout->read(2) + hal.rcout->read(3))/4);
// display input and output
//hal.console->printf("%d,%d,%d,%3.1f,%d,%d,%d,%d,%d,%d,%d,%d,%d\n", // octa
//hal.console->printf("%d,%d,%d,%3.1f,%d,%d,%d,%d,%d,%d,%d\n", // hexa
hal.console->printf("%d,%d,%d,%3.1f,%d,%d,%d,%d,%d\n", // quad
#if NUM_OUTPUTS <= 4
hal.console->printf("%d,%d,%d,%3.1f,%d,%d,%d,%d,%d\n", // quad
#elif NUM_OUTPUTS <= 6
hal.console->printf("%d,%d,%d,%3.1f,%d,%d,%d,%d,%d,%d,%d\n", // hexa
#else
hal.console->printf("%d,%d,%d,%3.1f,%d,%d,%d,%d,%d,%d,%d,%d,%d\n", // octa
#endif
(int)roll_in,
(int)pitch_in,
(int)yaw_in,
@ -170,10 +182,14 @@ void stability_test()
(int)hal.rcout->read(1),
(int)hal.rcout->read(2),
(int)hal.rcout->read(3),
//(int)hal.rcout->read(4),
//(int)hal.rcout->read(5),
//(int)hal.rcout->read(6),
//(int)hal.rcout->read(7),
#if NUM_OUTPUTS >= 6
(int)hal.rcout->read(4),
(int)hal.rcout->read(5),
#endif
#if NUM_OUTPUTS >= 8
(int)hal.rcout->read(6),
(int)hal.rcout->read(7),
#endif
(int)avg_out);
}
}