[44] | 1 | // created: 2016/06/01
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| 2 | // filename: PidUav.cpp
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| 3 | //
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| 4 | // author: Gildas Bayard
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| 5 | // Copyright Heudiasyc UMR UTC/CNRS 7253
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| 6 | //
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| 7 | // version: $Id: $
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| 8 | //
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| 9 | // purpose: Uav class showing the incidence of pid parameters choice
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| 10 | //
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| 11 | //
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| 12 | /*********************************************************************/
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| 13 |
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| 14 | #include "PidUav.h"
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| 15 | #include <TargetController.h>
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| 16 | #include <GridLayout.h>
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| 17 | #include <DataPlot1D.h>
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| 18 | #include <Tab.h>
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| 19 | #include <TabWidget.h>
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| 20 | #include <GroupBox.h>
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| 21 | #include <DoubleSpinBox.h>
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| 22 | #include <FrameworkManager.h>
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| 23 | #include <MetaDualShock3.h>
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| 24 | #include <Pid.h>
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| 25 | #include <AhrsData.h>
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| 26 |
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| 27 | #include <stdio.h>
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| 28 |
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| 29 | using namespace std;
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[105] | 30 | using namespace flair::core;
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| 31 | using namespace flair::sensor;
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| 32 | using namespace flair::gui;
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| 33 | using namespace flair::filter;
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| 34 | using namespace flair::meta;
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[44] | 35 |
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| 36 | /*
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| 37 | ** ===================================================================
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| 38 | ** constructor and destructor
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| 39 | **
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| 40 | ** ===================================================================
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| 41 | */
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[105] | 42 | PidUav::PidUav(Uav *uav, TargetController *controller)
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| 43 | : behaviourMode(BehaviourMode_t::Default),
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[236] | 44 | UavStateMachine(controller) {
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[105] | 45 | my_uRoll = new Pid(setupLawTab->At(1, 1), "custom uRoll");
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| 46 | my_uRoll->UseDefaultPlot(graphLawTab->LastRowLastCol());
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| 47 | my_uPitch = new Pid(setupLawTab->At(1, 0), "custom uPitch");
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| 48 | my_uPitch->UseDefaultPlot(graphLawTab->NewRow());
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[44] | 49 | }
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| 50 |
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| 51 | void PidUav::SignalEvent(Event_t event) {
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[105] | 52 | UavStateMachine::SignalEvent(event);
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| 53 | switch (event) {
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| 54 | case Event_t::TakingOff:
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| 55 | // always take off in default mode
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| 56 | behaviourMode = BehaviourMode_t::Default;
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| 57 | break;
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| 58 | case Event_t::EnteringFailSafeMode:
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| 59 | // return to default mode
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| 60 | Thread::Info("Entering failSafe mode\n");
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| 61 | behaviourMode = BehaviourMode_t::Default;
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| 62 | break;
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| 63 | }
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[44] | 64 | }
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| 65 |
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| 66 | bool PidUav::StartCustomMode() {
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[105] | 67 | // ask UavStateMachine to enter in custom torques
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| 68 | if (SetTorqueMode(TorqueMode_t::Custom)) {
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| 69 | Thread::Info("CustomTorques: start\n");
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| 70 | my_uPitch->Reset();
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| 71 | my_uRoll->Reset();
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| 72 | return true;
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| 73 | } else {
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| 74 | Thread::Warn("CustomTorques: could not start\n");
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| 75 | return false;
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| 76 | }
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[44] | 77 | }
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| 78 |
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| 79 | void PidUav::StartOscillatingMode() {
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[105] | 80 | if (behaviourMode == BehaviourMode_t::Default) {
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| 81 | if (!StartCustomMode())
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| 82 | return;
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| 83 | }
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| 84 | behaviourMode = BehaviourMode_t::Oscillating;
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| 85 | Thread::Info("Entering oscillating mode\n");
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| 86 | // remove the 'D' effect with a strong 'P'
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[44] | 87 | }
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| 88 |
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| 89 | void PidUav::ExtraCheckJoystick(void) {
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[105] | 90 | static bool wasOscillatingModeButtonPressed = false;
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| 91 | // controller button R1 enters optical flow mode
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[314] | 92 | if (GetTargetController()->IsButtonPressed(9)) { // R1
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[105] | 93 | if (!wasOscillatingModeButtonPressed) {
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| 94 | wasOscillatingModeButtonPressed = true;
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| 95 | if (behaviourMode != BehaviourMode_t::Oscillating)
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| 96 | StartOscillatingMode();
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[44] | 97 | }
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[105] | 98 | } else {
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| 99 | wasOscillatingModeButtonPressed = false;
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| 100 | }
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[44] | 101 | }
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| 102 |
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| 103 | void PidUav::ComputeCustomTorques(Euler &torques) {
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[105] | 104 | ComputeDefaultTorques(torques);
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| 105 | // overload default torques calculation for pitch and roll
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| 106 | const AhrsData *refOrientation = GetDefaultReferenceOrientation();
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| 107 | Quaternion refQuaternion;
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[236] | 108 | Vector3Df refAngularRates;
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[105] | 109 | refOrientation->GetQuaternionAndAngularRates(refQuaternion, refAngularRates);
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| 110 | Euler refAngles = refQuaternion.ToEuler();
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[44] | 111 |
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[105] | 112 | const AhrsData *currentOrientation = GetDefaultOrientation();
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| 113 | Quaternion currentQuaternion;
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[236] | 114 | Vector3Df currentAngularRates;
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[105] | 115 | currentOrientation->GetQuaternionAndAngularRates(currentQuaternion,
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| 116 | currentAngularRates);
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| 117 | Euler currentAngles = currentQuaternion.ToEuler();
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[44] | 118 |
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[105] | 119 | my_uRoll->SetValues(currentAngles.roll - refAngles.roll,
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| 120 | currentAngularRates.x);
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| 121 | my_uRoll->Update(GetTime());
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| 122 | torques.roll = my_uRoll->Output();
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[44] | 123 |
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[105] | 124 | my_uPitch->SetValues(currentAngles.pitch - refAngles.pitch,
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| 125 | currentAngularRates.y);
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| 126 | my_uPitch->Update(GetTime());
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| 127 | torques.pitch = my_uPitch->Output();
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[44] | 128 | }
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| 129 |
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[105] | 130 | PidUav::~PidUav() {}
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