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Copter: add takeoff comments

master
Randy Mackay 10 years ago
parent
commit
70f9739d77
  1. 15
      ArduCopter/takeoff.pde

15
ArduCopter/takeoff.pde

@ -1,6 +1,12 @@ @@ -1,6 +1,12 @@
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
// This file contains the high-level takeoff logic for Loiter, PosHold, AltHold, Sport modes.
// The take-off can be initiated from a GCS NAV_TAKEOFF command which includes a takeoff altitude
// A safe takeoff speed is calculated and used to calculate a time_ms
// the pos_control target is then slowly increased until time_ms expires
// return true if this flight mode supports user takeoff
// must_nagivate is true if mode must also control horizontal position
bool current_mode_has_user_takeoff(bool with_navigation)
{
switch (control_mode) {
@ -16,6 +22,7 @@ bool current_mode_has_user_takeoff(bool with_navigation) @@ -16,6 +22,7 @@ bool current_mode_has_user_takeoff(bool with_navigation)
}
}
// initiate user takeoff - called when MAVLink TAKEOFF command is received
static bool do_user_takeoff(float takeoff_alt_cm, bool must_navigate)
{
if (motors.armed() && ap.land_complete && current_mode_has_user_takeoff(must_navigate) && takeoff_alt_cm > current_loc.alt) {
@ -36,20 +43,25 @@ static bool do_user_takeoff(float takeoff_alt_cm, bool must_navigate) @@ -36,20 +43,25 @@ static bool do_user_takeoff(float takeoff_alt_cm, bool must_navigate)
return false;
}
// start takeoff to specified altitude above home
static void takeoff_timer_start(float alt)
{
// calculate climb rate
float speed = min(wp_nav.get_speed_up(), max(g.pilot_velocity_z_max*2.0f/3.0f, g.pilot_velocity_z_max-50.0f));
// sanity check speed and target
if (takeoff_state.running || speed <= 0.0f || alt <= 0.0f) {
return;
}
// initialise takeoff state
takeoff_state.running = true;
takeoff_state.speed = speed;
takeoff_state.start_ms = millis();
takeoff_state.time_ms = (alt/takeoff_state.speed) * 1.0e3f;
}
// update takeoff timer and stop the takeoff after time_ms has passed
static void takeoff_timer_update()
{
if (millis()-takeoff_state.start_ms >= takeoff_state.time_ms) {
@ -57,6 +69,8 @@ static void takeoff_timer_update() @@ -57,6 +69,8 @@ static void takeoff_timer_update()
}
}
// increase altitude target as part of takeoff
// dt - time interval (in seconds) that this function is called
static void takeoff_increment_alt_target(float dt)
{
if (takeoff_state.running) {
@ -66,6 +80,7 @@ static void takeoff_increment_alt_target(float dt) @@ -66,6 +80,7 @@ static void takeoff_increment_alt_target(float dt)
}
}
// get take off speed in cm/s
static float takeoff_get_speed()
{
return takeoff_state.running?takeoff_state.speed:0.0f;

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