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#include "UASUnitTest.h"
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UASUnitTest::UASUnitTest()
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{
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}
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void UASUnitTest::initTestCase()
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{
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mav= new MAVLinkProtocol();
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link = new SerialLink();
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uas=new UAS(mav,UASID);
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}
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void UASUnitTest::cleanupTestCase()
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{
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delete uas;
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delete mav;
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}
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void UASUnitTest::getUASID_test()
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{
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// Test a default ID of zero is assigned
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UAS* uas2 = new UAS(mav);
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QCOMPARE(uas2->getUASID(), 0);
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delete uas2;
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// Test that the chosen ID was assigned at construction
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QCOMPARE(uas->getUASID(), UASID);
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// Make sure that no other ID was sert
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QEXPECT_FAIL("", "When you set an ID it does not use the default ID of 0", Continue);
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QCOMPARE(uas->getUASID(), 0);
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}
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void UASUnitTest::getUASName_test()
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{
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// Test that the name is build as MAV + ID
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QCOMPARE(uas->getUASName(), "MAV 0" + QString::number(UASID));
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}
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void UASUnitTest::getUpTime_test()
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{
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UAS* uas2 = new UAS(mav);
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// Test that the uptime starts at zero to a
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// precision of seconds
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QCOMPARE(floor(uas2->getUptime()/1000.0), 0.0);
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// Sleep for three seconds
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QTest::qSleep(3000);
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// Test that the up time is computed correctly to a
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// precision of seconds
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QCOMPARE(floor(uas2->getUptime()/1000.0), 3.0);
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delete uas2;
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}
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void UASUnitTest::getCommunicationStatus_test()
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{
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// Verify that upon construction the Comm status is disconnected
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QCOMPARE(uas->getCommunicationStatus(), static_cast<int>(UASInterface::COMM_DISCONNECTED));
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}
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void UASUnitTest::filterVoltage_test()
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{
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float verificar=uas->filterVoltage(0.4f);
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// Verify that upon construction the Comm status is disconnected
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QCOMPARE(verificar, 8.52f);
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}
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void UASUnitTest:: getAutopilotType_test()
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{
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int type = uas->getAutopilotType();
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// Verify that upon construction the autopilot is set to -1
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QCOMPARE(type, -1);
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}
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void UASUnitTest::setAutopilotType_test()
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{
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uas->setAutopilotType(2);
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// Verify that the autopilot is set
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QCOMPARE(uas->getAutopilotType(), 2);
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}
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void UASUnitTest::getStatusForCode_test()
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{
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QString state, desc;
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state = "";
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desc = "";
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uas->getStatusForCode(MAV_STATE_UNINIT, state, desc);
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QVERIFY(state == "UNINIT");
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uas->getStatusForCode(MAV_STATE_UNINIT, state, desc);
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QVERIFY(state == "UNINIT");
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uas->getStatusForCode(MAV_STATE_BOOT, state, desc);
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QVERIFY(state == "BOOT");
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uas->getStatusForCode(MAV_STATE_CALIBRATING, state, desc);
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QVERIFY(state == "CALIBRATING");
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uas->getStatusForCode(MAV_STATE_ACTIVE, state, desc);
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QVERIFY(state == "ACTIVE");
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uas->getStatusForCode(MAV_STATE_STANDBY, state, desc);
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QVERIFY(state == "STANDBY");
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uas->getStatusForCode(MAV_STATE_CRITICAL, state, desc);
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QVERIFY(state == "CRITICAL");
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uas->getStatusForCode(MAV_STATE_EMERGENCY, state, desc);
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QVERIFY(state == "EMERGENCY");
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uas->getStatusForCode(MAV_STATE_POWEROFF, state, desc);
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QVERIFY(state == "SHUTDOWN");
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uas->getStatusForCode(5325, state, desc);
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QVERIFY(state == "UNKNOWN");
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}
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void UASUnitTest::getLocalX_test()
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{
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QCOMPARE(uas->getLocalX(), 0.0);
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}
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void UASUnitTest::getLocalY_test()
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{
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QCOMPARE(uas->getLocalY(), 0.0);
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}
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void UASUnitTest::getLocalZ_test()
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{
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QCOMPARE(uas->getLocalZ(), 0.0);
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}
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void UASUnitTest::getLatitude_test()
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{ QCOMPARE(uas->getLatitude(), 0.0);
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}
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void UASUnitTest::getLongitude_test()
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{
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QCOMPARE(uas->getLongitude(), 0.0);
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}
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void UASUnitTest::getAltitude_test()
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{
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QCOMPARE(uas->getAltitude(), 0.0);
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}
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void UASUnitTest::getRoll_test()
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{
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QCOMPARE(uas->getRoll(), 0.0);
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}
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void UASUnitTest::getPitch_test()
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{
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QCOMPARE(uas->getPitch(), 0.0);
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}
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void UASUnitTest::getYaw_test()
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{
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QCOMPARE(uas->getYaw(), 0.0);
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}
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void UASUnitTest::attitudeLimitsZero_test()
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{
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mavlink_message_t msg;
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mavlink_attitude_t att;
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// Set zero values and encode them
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att.roll = 0.0f;
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att.pitch = 0.0f;
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att.yaw = 0.0f;
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mavlink_msg_attitude_encode(uas->getUASID(), MAV_COMP_ID_IMU, &msg, &att);
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// Let UAS decode message
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uas->receiveMessage(link, msg);
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// Check result
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QCOMPARE(uas->getRoll(), 0.0);
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QCOMPARE(uas->getPitch(), 0.0);
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QCOMPARE(uas->getYaw(), 0.0);
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}
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void UASUnitTest::attitudeLimitsPi_test()
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{
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mavlink_message_t msg;
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mavlink_attitude_t att;
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// Set PI values and encode them
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att.roll = M_PI;
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att.pitch = M_PI;
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att.yaw = M_PI;
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mavlink_msg_attitude_encode(uas->getUASID(), MAV_COMP_ID_IMU, &msg, &att);
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// Let UAS decode message
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uas->receiveMessage(link, msg);
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// Check result
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QVERIFY((uas->getRoll() < M_PI+0.000001) && (uas->getRoll() > M_PI+-0.000001));
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QVERIFY((uas->getPitch() < M_PI+0.000001) && (uas->getPitch() > M_PI+-0.000001));
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QVERIFY((uas->getYaw() < M_PI+0.000001) && (uas->getYaw() > M_PI+-0.000001));
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}
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void UASUnitTest::attitudeLimitsMinusPi_test()
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{
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mavlink_message_t msg;
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mavlink_attitude_t att;
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// Set -PI values and encode them
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att.roll = -M_PI;
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att.pitch = -M_PI;
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att.yaw = -M_PI;
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mavlink_msg_attitude_encode(uas->getUASID(), MAV_COMP_ID_IMU, &msg, &att);
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// Let UAS decode message
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uas->receiveMessage(link, msg);
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// Check result
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QVERIFY((uas->getRoll() > -M_PI-0.000001) && (uas->getRoll() < -M_PI+0.000001));
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QVERIFY((uas->getPitch() > -M_PI-0.000001) && (uas->getPitch() < -M_PI+0.000001));
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QVERIFY((uas->getYaw() > -M_PI-0.000001) && (uas->getYaw() < -M_PI+0.000001));
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}
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void UASUnitTest::attitudeLimitsTwoPi_test()
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{
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mavlink_message_t msg;
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mavlink_attitude_t att;
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// Set off-limit values and check
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// correct wrapping
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// Set 2PI values and encode them
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att.roll = 2*M_PI;
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att.pitch = 2*M_PI;
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att.yaw = 2*M_PI;
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mavlink_msg_attitude_encode(uas->getUASID(), MAV_COMP_ID_IMU, &msg, &att);
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// Let UAS decode message
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uas->receiveMessage(link, msg);
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// Check result
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QVERIFY((uas->getRoll() < 0.000001) && (uas->getRoll() > -0.000001));
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QVERIFY((uas->getPitch() < 0.000001) && (uas->getPitch() > -0.000001));
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QVERIFY((uas->getYaw() < 0.000001) && (uas->getYaw() > -0.000001));
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}
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void UASUnitTest::attitudeLimitsMinusTwoPi_test()
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{
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mavlink_message_t msg;
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mavlink_attitude_t att;
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// Set -2PI values and encode them
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att.roll = -2*M_PI;
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att.pitch = -2*M_PI;
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att.yaw = -2*M_PI;
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mavlink_msg_attitude_encode(uas->getUASID(), MAV_COMP_ID_IMU, &msg, &att);
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// Let UAS decode message
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uas->receiveMessage(link, msg);
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// Check result
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QVERIFY((uas->getRoll() < 0.000001) && (uas->getRoll() > -0.000001));
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QVERIFY((uas->getPitch() < 0.000001) && (uas->getPitch() > -0.000001));
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QVERIFY((uas->getYaw() < 0.000001) && (uas->getYaw() > -0.000001));
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}
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void UASUnitTest::attitudeLimitsTwoPiOne_test()
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{
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mavlink_message_t msg;
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mavlink_attitude_t att;
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// Set over 2 PI values and encode them
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att.roll = 2*M_PI+1.0f;
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att.pitch = 2*M_PI+1.0f;
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att.yaw = 2*M_PI+1.0f;
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mavlink_msg_attitude_encode(uas->getUASID(), MAV_COMP_ID_IMU, &msg, &att);
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// Let UAS decode message
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uas->receiveMessage(link, msg);
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// Check result
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QVERIFY((uas->getRoll() < 1.000001) && (uas->getRoll() > 0.999999));
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QVERIFY((uas->getPitch() < 1.000001) && (uas->getPitch() > 0.999999));
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QVERIFY((uas->getYaw() < 1.000001) && (uas->getYaw() > 0.999999));
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}
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void UASUnitTest::attitudeLimitsMinusTwoPiOne_test()
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{
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mavlink_message_t msg;
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mavlink_attitude_t att;
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// Set 3PI values and encode them
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att.roll = -2*M_PI-1.0f;
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att.pitch = -2*M_PI-1.0f;
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att.yaw = -2*M_PI-1.0f;
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mavlink_msg_attitude_encode(uas->getUASID(), MAV_COMP_ID_IMU, &msg, &att);
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// Let UAS decode message
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uas->receiveMessage(link, msg);
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// Check result
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QVERIFY((uas->getRoll() > -1.000001) && (uas->getRoll() < -0.999999));
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QVERIFY((uas->getPitch() > -1.000001) && (uas->getPitch() < -0.999999));
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QVERIFY((uas->getYaw() > -1.000001) && (uas->getYaw() < -0.999999));
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}
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