ardupilot/ArduPlane/control_modes.pde
Andrew Tridgell 526344ab7c APM: added control switch debouncer
this adds a switch debouncer, similar to the one used in
ArduCopter. I'm adding this after a flight on the weekend where noise
on the control mode channel caused a mode change away from auto.

To prevent this change adding excessive mode switch latency, it also
moves the reading of the control switch to the 10Hz loop, away from
the 3.3Hz loop. That gives us 0.2s delay in mode switch changes and
allows for spikes in the control mode for 0.1 seconds without changing
mode.
2012-08-01 13:59:37 +10:00

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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
static void read_control_switch()
{
static bool switch_debouncer;
byte switchPosition = readSwitch();
// If switchPosition = 255 this indicates that the mode control channel input was out of range
// If we get this value we do not want to change modes.
if(switchPosition == 255) return;
// we look for changes in the switch position. If the
// RST_SWITCH_CH parameter is set, then it is a switch that can be
// used to force re-reading of the control switch. This is useful
// when returning to the previous mode after a failsafe or fence
// breach. This channel is best used on a momentary switch (such
// as a spring loaded trainer switch).
if (oldSwitchPosition != switchPosition ||
(g.reset_switch_chan != 0 &&
APM_RC.InputCh(g.reset_switch_chan-1) > RESET_SWITCH_CHAN_PWM)) {
if (switch_debouncer == false) {
// this ensures that mode switches only happen if the
// switch changes for 2 reads. This prevents momentary
// spikes in the mode control channel from causing a mode
// switch
switch_debouncer = true;
return;
}
set_mode(flight_modes[switchPosition]);
oldSwitchPosition = switchPosition;
prev_WP = current_loc;
// reset navigation integrators
// -------------------------
reset_I();
}
switch_debouncer = false;
if (g.inverted_flight_ch != 0) {
// if the user has configured an inverted flight channel, then
// fly upside down when that channel goes above INVERTED_FLIGHT_PWM
inverted_flight = (control_mode != MANUAL && APM_RC.InputCh(g.inverted_flight_ch-1) > INVERTED_FLIGHT_PWM);
}
}
static byte readSwitch(void){
uint16_t pulsewidth = APM_RC.InputCh(g.flight_mode_channel - 1);
if (pulsewidth <= 910 || pulsewidth >= 2090) return 255; // This is an error condition
if (pulsewidth > 1230 && pulsewidth <= 1360) return 1;
if (pulsewidth > 1360 && pulsewidth <= 1490) return 2;
if (pulsewidth > 1490 && pulsewidth <= 1620) return 3;
if (pulsewidth > 1620 && pulsewidth <= 1749) return 4; // Software Manual
if (pulsewidth >= 1750) return 5; // Hardware Manual
return 0;
}
static void reset_control_switch()
{
oldSwitchPosition = 0;
read_control_switch();
}
static void update_servo_switches()
{
#if CONFIG_APM_HARDWARE != APM_HARDWARE_APM2
if (!g.switch_enable) {
// switches are disabled in EEPROM (see SWITCH_ENABLE option)
// this means the EEPROM control of all channel reversal is enabled
return;
}
// up is reverse
// up is elevon
g.mix_mode = (PINL & 128) ? 1 : 0; // 1 for elevon mode
if (g.mix_mode == 0) {
g.channel_roll.set_reverse((PINE & 128) ? true : false);
g.channel_pitch.set_reverse((PINE & 64) ? true : false);
g.channel_rudder.set_reverse((PINL & 64) ? true : false);
} else {
g.reverse_elevons = (PINE & 128) ? true : false;
g.reverse_ch1_elevon = (PINE & 64) ? true : false;
g.reverse_ch2_elevon = (PINL & 64) ? true : false;
}
#endif
}