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