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