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Copter: remove tune from cli to save 300bytes flash

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This commit is contained in:
Randy Mackay 2013-09-23 23:38:36 +09:00
parent 1cc2c8d6a5
commit d7782e1356
2 changed files with 0 additions and 80 deletions
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10
ArduCopter/setup.pde
View File

@ -23,7 +23,6 @@ static int8_t setup_factory (uint8_t argc, const Menu::arg *argv);
static int8_t setup_set (uint8_t argc, const Menu::arg *argv);
static int8_t setup_show (uint8_t argc, const Menu::arg *argv);
static int8_t setup_sonar (uint8_t argc, const Menu::arg *argv);
static int8_t setup_tune (uint8_t argc, const Menu::arg *argv);
// Command/function table for the setup menu
@ -50,7 +49,6 @@ const struct Menu::command setup_menu_commands[] PROGMEM = {
{"set", setup_set},
{"show", setup_show},
{"sonar", setup_sonar},
{"tune", setup_tune}
};
// Create the setup menu object.
@ -1005,14 +1003,6 @@ setup_sonar(uint8_t argc, const Menu::arg *argv)
return 0;
}
static int8_t
setup_tune(uint8_t argc, const Menu::arg *argv)
{
g.radio_tuning.set_and_save(argv[1].i);
report_tuning();
return 0;
}
/***************************************************************************/
// CLI reports
/***************************************************************************/

70
ArduCopter/test.pde
View File

@ -23,8 +23,6 @@ static int8_t test_shell(uint8_t argc, const Menu::arg *argv);
#if HIL_MODE != HIL_MODE_ATTITUDE && HIL_MODE != HIL_MODE_SENSORS
static int8_t test_sonar(uint8_t argc, const Menu::arg *argv);
#endif
//static int8_t test_toy(uint8_t argc, const Menu::arg *argv);
static int8_t test_tuning(uint8_t argc, const Menu::arg *argv);
// This is the help function
// PSTR is an AVR macro to read strings from flash memory
@ -65,8 +63,6 @@ const struct Menu::command test_menu_commands[] PROGMEM = {
#if HIL_MODE != HIL_MODE_ATTITUDE && HIL_MODE != HIL_MODE_SENSORS
{"sonar", test_sonar},
#endif
// {"toy", test_toy},
{"tune", test_tuning}
};
// A Macro to create the Menu
@ -513,72 +509,6 @@ test_sonar(uint8_t argc, const Menu::arg *argv)
}
#endif
/*
//static int8_t
//test_toy(uint8_t argc, const Menu::arg *argv)
{
for(altitude_error = 2000; altitude_error > -100; altitude_error--){
int16_t temp = get_desired_climb_rate();
cliSerial->printf("%ld, %d\n", altitude_error, temp);
}
return 0;
}
{ wp_distance = 0;
int16_t max_speed = 0;
for(int16_t i = 0; i < 200; i++){
int32_t temp = 2 * 100 * (wp_distance - wp_nav.get_waypoint_radius());
max_speed = sqrtf((float)temp);
max_speed = min(max_speed, wp_nav.get_horizontal_speed());
cliSerial->printf("Zspeed: %ld, %d, %ld\n", temp, max_speed, wp_distance);
wp_distance += 100;
}
return 0;
}
//*/
/*static int8_t
* //test_toy(uint8_t argc, const Menu::arg *argv)
* {
* int16_t yaw_rate;
* int16_t roll_rate;
* g.rc_1.control_in = -2500;
* g.rc_2.control_in = 2500;
*
* g.toy_yaw_rate = 3;
* yaw_rate = g.rc_1.control_in / g.toy_yaw_rate;
* roll_rate = ((int32_t)g.rc_2.control_in * (yaw_rate/100)) /40;
* cliSerial->printf("yaw_rate, %d, roll_rate, %d\n", yaw_rate, roll_rate);
*
* g.toy_yaw_rate = 2;
* yaw_rate = g.rc_1.control_in / g.toy_yaw_rate;
* roll_rate = ((int32_t)g.rc_2.control_in * (yaw_rate/100)) /40;
* cliSerial->printf("yaw_rate, %d, roll_rate, %d\n", yaw_rate, roll_rate);
*
* g.toy_yaw_rate = 1;
* yaw_rate = g.rc_1.control_in / g.toy_yaw_rate;
* roll_rate = ((int32_t)g.rc_2.control_in * (yaw_rate/100)) /40;
* cliSerial->printf("yaw_rate, %d, roll_rate, %d\n", yaw_rate, roll_rate);
* }*/
static int8_t
test_tuning(uint8_t argc, const Menu::arg *argv)
{
print_hit_enter();
while(1) {
delay(200);
read_radio();
tuning();
cliSerial->printf_P(PSTR("tune: %1.3f\n"), tuning_value);
if(cliSerial->available() > 0) {
return (0);
}
}
}
static void print_hit_enter()
{
cliSerial->printf_P(PSTR("Hit Enter to exit.\n\n"));