Added interactive control for altitude in Loiter (position hold) and Altitude hold (mostly just used for testing).
Throttle down = descend, throttle high = ascend. git-svn-id: https://arducopter.googlecode.com/svn/trunk@1831 f9c3cf11-9bcb-44bc-f272-b75c42450872
This commit is contained in:
parent
294d6752fe
commit
72fc8a1f51
@ -416,7 +416,7 @@ uint8_t delta_ms_medium_loop;
|
||||
|
||||
byte slow_loopCounter;
|
||||
int superslow_loopCounter;
|
||||
byte fbw_timer; // for limiting the execution of FBW input
|
||||
byte flight_timer; // for limiting the execution of flight mode thingys
|
||||
|
||||
//unsigned long nav_loopTimer; // used to track the elapsed ime for GPS nav
|
||||
unsigned long nav2_loopTimer; // used to track the elapsed ime for GPS nav
|
||||
@ -919,10 +919,10 @@ void update_current_flight_mode(void)
|
||||
break;
|
||||
|
||||
case SIMPLE:
|
||||
fbw_timer++;
|
||||
flight_timer++;
|
||||
// 25 hz
|
||||
if(fbw_timer > 4){
|
||||
fbw_timer = 0;
|
||||
if(flight_timer > 4){
|
||||
flight_timer = 0;
|
||||
|
||||
current_loc.lat = 0;
|
||||
current_loc.lng = 0;
|
||||
@ -966,11 +966,11 @@ void update_current_flight_mode(void)
|
||||
|
||||
case FBW:
|
||||
// we are currently using manual throttle during alpha testing.
|
||||
fbw_timer++;
|
||||
flight_timer++;
|
||||
|
||||
// 10 hz
|
||||
if(fbw_timer > 10){
|
||||
fbw_timer = 0;
|
||||
if(flight_timer > 10){
|
||||
flight_timer = 0;
|
||||
|
||||
if(GPS_disabled){
|
||||
current_loc.lat = home.lat = 0;
|
||||
@ -1010,9 +1010,20 @@ void update_current_flight_mode(void)
|
||||
|
||||
//if(g.rc_3.control_in)
|
||||
// get desired height from the throttle
|
||||
next_WP.alt = home.alt + (g.rc_3.control_in); // 0 - 1000 (40 meters)
|
||||
next_WP.alt = max(next_WP.alt, 30);
|
||||
//next_WP.alt = home.alt + (g.rc_3.control_in); // 0 - 1000 (40 meters)
|
||||
//next_WP.alt = max(next_WP.alt, 30);
|
||||
|
||||
flight_timer++;
|
||||
|
||||
if(flight_timer >= 2){
|
||||
flight_timer = 0;
|
||||
|
||||
if(g.rc_3.control_in <= 0){
|
||||
next_WP.alt -= 1;
|
||||
}else if (g.rc_3.control_in > 700){
|
||||
next_WP.alt += 1;
|
||||
}
|
||||
}
|
||||
// !!! testing
|
||||
//next_WP.alt -= 500;
|
||||
|
||||
@ -1051,10 +1062,23 @@ void update_current_flight_mode(void)
|
||||
|
||||
case LOITER:
|
||||
|
||||
flight_timer++;
|
||||
|
||||
if(flight_timer >= 2){
|
||||
flight_timer = 0;
|
||||
|
||||
if(g.rc_3.control_in <= 0){
|
||||
next_WP.alt -= 1;
|
||||
}else if (g.rc_3.control_in > 700){
|
||||
next_WP.alt += 1;
|
||||
}
|
||||
}
|
||||
|
||||
// Yaw control
|
||||
// -----------
|
||||
output_manual_yaw();
|
||||
|
||||
|
||||
// Output Pitch, Roll, Yaw and Throttle
|
||||
// ------------------------------------
|
||||
|
||||
|
Loading…
Reference in New Issue
Block a user