ardupilot/ArduSub/control_manual.cpp

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2016-06-26 01:07:27 -03:00
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#include "Sub.h"
// manual_init - initialise manual controller
bool Sub::manual_init(bool ignore_checks)
{
// if landed and the mode we're switching from does not have manual throttle and the throttle stick is too high
if (motors.armed() && ap.land_complete && !mode_has_manual_throttle(control_mode) && (get_pilot_desired_throttle(channel_throttle->get_control_in()) > get_non_takeoff_throttle())) {
return false;
}
// set target altitude to zero for reporting
pos_control.set_alt_target(0);
return true;
}
// manual_run - runs the manual (passthrough) controller
// should be called at 100hz or more
void Sub::manual_run()
{
// if not armed set throttle to zero and exit immediately
if (!motors.armed() || !motors.get_interlock()) {
motors.set_desired_spool_state(AP_Motors::DESIRED_SPIN_WHEN_ARMED);
attitude_control.set_throttle_out_unstabilized(0,true,g.throttle_filt);
return;
}
motors.set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);
motors.set_roll(channel_roll->norm_input_dz()*0.67f);
motors.set_pitch(channel_pitch->norm_input_dz()*0.67f);
motors.set_yaw(channel_yaw->norm_input_dz()*0.67f);
motors.set_throttle(channel_throttle->norm_input_dz());
motors.set_forward(channel_forward->norm_input_dz()*0.67f);
motors.set_lateral(channel_lateral->norm_input_dz()*0.67f);
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}