|
|
|
@ -43,32 +43,32 @@ TEST(PositionControlTest, EmptySetpoint)
@@ -43,32 +43,32 @@ TEST(PositionControlTest, EmptySetpoint)
|
|
|
|
|
|
|
|
|
|
vehicle_local_position_setpoint_s output_setpoint{}; |
|
|
|
|
position_control.getLocalPositionSetpoint(output_setpoint); |
|
|
|
|
EXPECT_EQ(output_setpoint.x, 0); |
|
|
|
|
EXPECT_EQ(output_setpoint.y, 0); |
|
|
|
|
EXPECT_EQ(output_setpoint.z, 0); |
|
|
|
|
EXPECT_EQ(output_setpoint.yaw, 0); |
|
|
|
|
EXPECT_EQ(output_setpoint.yawspeed, 0); |
|
|
|
|
EXPECT_EQ(output_setpoint.vx, 0); |
|
|
|
|
EXPECT_EQ(output_setpoint.vy, 0); |
|
|
|
|
EXPECT_EQ(output_setpoint.vz, 0); |
|
|
|
|
EXPECT_EQ(Vector3f(output_setpoint.acceleration), Vector3f(0, 0, 0)); |
|
|
|
|
EXPECT_EQ(Vector3f(output_setpoint.jerk), Vector3f(0, 0, 0)); |
|
|
|
|
EXPECT_EQ(output_setpoint.x, 0.f); |
|
|
|
|
EXPECT_EQ(output_setpoint.y, 0.f); |
|
|
|
|
EXPECT_EQ(output_setpoint.z, 0.f); |
|
|
|
|
EXPECT_EQ(output_setpoint.yaw, 0.f); |
|
|
|
|
EXPECT_EQ(output_setpoint.yawspeed, 0.f); |
|
|
|
|
EXPECT_EQ(output_setpoint.vx, 0.f); |
|
|
|
|
EXPECT_EQ(output_setpoint.vy, 0.f); |
|
|
|
|
EXPECT_EQ(output_setpoint.vz, 0.f); |
|
|
|
|
EXPECT_EQ(Vector3f(output_setpoint.acceleration), Vector3f(0.f, 0.f, 0.f)); |
|
|
|
|
EXPECT_EQ(Vector3f(output_setpoint.jerk), Vector3f(0.f, 0.f, 0.f)); |
|
|
|
|
EXPECT_EQ(Vector3f(output_setpoint.thrust), Vector3f(0, 0, 0)); |
|
|
|
|
|
|
|
|
|
vehicle_attitude_setpoint_s attitude{}; |
|
|
|
|
position_control.getAttitudeSetpoint(attitude); |
|
|
|
|
EXPECT_EQ(attitude.roll_body, 0); |
|
|
|
|
EXPECT_EQ(attitude.pitch_body, 0); |
|
|
|
|
EXPECT_EQ(attitude.yaw_body, 0); |
|
|
|
|
EXPECT_EQ(attitude.yaw_sp_move_rate, 0); |
|
|
|
|
EXPECT_EQ(Quatf(attitude.q_d), Quatf(1, 0, 0, 0)); |
|
|
|
|
EXPECT_EQ(attitude.roll_body, 0.f); |
|
|
|
|
EXPECT_EQ(attitude.pitch_body, 0.f); |
|
|
|
|
EXPECT_EQ(attitude.yaw_body, 0.f); |
|
|
|
|
EXPECT_EQ(attitude.yaw_sp_move_rate, 0.f); |
|
|
|
|
EXPECT_EQ(Quatf(attitude.q_d), Quatf(1.f, 0.f, 0.f, 0.f)); |
|
|
|
|
//EXPECT_EQ(attitude.q_d_valid, false); // TODO should not be true when there was no control
|
|
|
|
|
EXPECT_EQ(Vector3f(attitude.thrust_body), Vector3f(0, 0, 0)); |
|
|
|
|
EXPECT_EQ(Vector3f(attitude.thrust_body), Vector3f(0.f, 0.f, 0.f)); |
|
|
|
|
EXPECT_EQ(attitude.roll_reset_integral, false); |
|
|
|
|
EXPECT_EQ(attitude.pitch_reset_integral, false); |
|
|
|
|
EXPECT_EQ(attitude.yaw_reset_integral, false); |
|
|
|
|
EXPECT_EQ(attitude.fw_control_yaw, false); |
|
|
|
|
EXPECT_EQ(attitude.apply_flaps, 0);//vehicle_attitude_setpoint_s::FLAPS_OFF); // TODO why no reference?
|
|
|
|
|
EXPECT_EQ(attitude.apply_flaps, 0.f);//vehicle_attitude_setpoint_s::FLAPS_OFF); // TODO why no reference?
|
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
class PositionControlBasicTest : public ::testing::Test |
|
|
|
@ -76,11 +76,11 @@ class PositionControlBasicTest : public ::testing::Test
@@ -76,11 +76,11 @@ class PositionControlBasicTest : public ::testing::Test
|
|
|
|
|
public: |
|
|
|
|
PositionControlBasicTest() |
|
|
|
|
{ |
|
|
|
|
_position_control.setPositionGains(Vector3f(1, 1, 1)); |
|
|
|
|
_position_control.setVelocityGains(Vector3f(1, 1, 1), Vector3f(1, 1, 1), Vector3f(1, 1, 1)); |
|
|
|
|
_position_control.setVelocityLimits(1, 1, 1); |
|
|
|
|
_position_control.setPositionGains(Vector3f(1.f, 1.f, 1.f)); |
|
|
|
|
_position_control.setVelocityGains(Vector3f(1.f, 1.f, 1.f), Vector3f(1.f, 1.f, 1.f), Vector3f(1.f, 1.f, 1.f)); |
|
|
|
|
_position_control.setVelocityLimits(1.f, 1.f, 1.f); |
|
|
|
|
_position_control.setThrustLimits(0.1f, 0.9f); |
|
|
|
|
_position_control.setTiltLimit(1); |
|
|
|
|
_position_control.setTiltLimit(1.f); |
|
|
|
|
_position_control.setHoverThrust(.5f); |
|
|
|
|
|
|
|
|
|
_contraints.tilt = 1.f; |
|
|
|
@ -122,14 +122,14 @@ public:
@@ -122,14 +122,14 @@ public:
|
|
|
|
|
void checkDirection() |
|
|
|
|
{ |
|
|
|
|
Vector3f thrust(_output_setpoint.thrust); |
|
|
|
|
EXPECT_GT(thrust(0), 0); |
|
|
|
|
EXPECT_GT(thrust(1), 0); |
|
|
|
|
EXPECT_LT(thrust(2), 0); |
|
|
|
|
EXPECT_GT(thrust(0), 0.f); |
|
|
|
|
EXPECT_GT(thrust(1), 0.f); |
|
|
|
|
EXPECT_LT(thrust(2), 0.f); |
|
|
|
|
|
|
|
|
|
Vector3f body_z = Quatf(_attitude.q_d).dcm_z(); |
|
|
|
|
EXPECT_LT(body_z(0), 0); |
|
|
|
|
EXPECT_LT(body_z(1), 0); |
|
|
|
|
EXPECT_GT(body_z(2), 0); |
|
|
|
|
EXPECT_LT(body_z(0), 0.f); |
|
|
|
|
EXPECT_LT(body_z(1), 0.f); |
|
|
|
|
EXPECT_GT(body_z(2), 0.f); |
|
|
|
|
} |
|
|
|
|
}; |
|
|
|
|
|
|
|
|
@ -153,41 +153,41 @@ TEST_F(PositionControlBasicDirectionTest, VelocityControlDirection)
@@ -153,41 +153,41 @@ TEST_F(PositionControlBasicDirectionTest, VelocityControlDirection)
|
|
|
|
|
|
|
|
|
|
TEST_F(PositionControlBasicTest, PositionControlMaxTilt) |
|
|
|
|
{ |
|
|
|
|
_input_setpoint.x = 10; |
|
|
|
|
_input_setpoint.y = 10; |
|
|
|
|
_input_setpoint.z = -0; |
|
|
|
|
_input_setpoint.x = 10.f; |
|
|
|
|
_input_setpoint.y = 10.f; |
|
|
|
|
_input_setpoint.z = -0.f; |
|
|
|
|
|
|
|
|
|
runController(); |
|
|
|
|
Vector3f body_z = Quatf(_attitude.q_d).dcm_z(); |
|
|
|
|
float angle = acosf(body_z.dot(Vector3f(0, 0, 1))); |
|
|
|
|
float angle = acosf(body_z.dot(Vector3f(0.f, 0.f, 1.f))); |
|
|
|
|
EXPECT_GT(angle, 0.f); |
|
|
|
|
EXPECT_LE(angle, 1.f); |
|
|
|
|
|
|
|
|
|
_contraints.tilt = .5f; |
|
|
|
|
runController(); |
|
|
|
|
body_z = Quatf(_attitude.q_d).dcm_z(); |
|
|
|
|
angle = acosf(body_z.dot(Vector3f(0, 0, 1))); |
|
|
|
|
angle = acosf(body_z.dot(Vector3f(0.f, 0.f, 1.f))); |
|
|
|
|
EXPECT_GT(angle, 0.f); |
|
|
|
|
EXPECT_LE(angle, .50001f); |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
TEST_F(PositionControlBasicTest, PositionControlMaxVelocity) |
|
|
|
|
{ |
|
|
|
|
_input_setpoint.x = 10; |
|
|
|
|
_input_setpoint.y = 10; |
|
|
|
|
_input_setpoint.z = -10; |
|
|
|
|
_input_setpoint.x = 10.f; |
|
|
|
|
_input_setpoint.y = 10.f; |
|
|
|
|
_input_setpoint.z = -10.f; |
|
|
|
|
|
|
|
|
|
runController(); |
|
|
|
|
Vector2f velocity_xy(_output_setpoint.vx, _output_setpoint.vy); |
|
|
|
|
EXPECT_LE(velocity_xy.norm(), 1); |
|
|
|
|
EXPECT_LE(abs(_output_setpoint.vz), 1); |
|
|
|
|
EXPECT_LE(velocity_xy.norm(), 1.f); |
|
|
|
|
EXPECT_LE(abs(_output_setpoint.vz), 1.f); |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
TEST_F(PositionControlBasicTest, PositionControlThrustLimit) |
|
|
|
|
{ |
|
|
|
|
_input_setpoint.x = 10; |
|
|
|
|
_input_setpoint.y = 10; |
|
|
|
|
_input_setpoint.z = -10; |
|
|
|
|
_input_setpoint.x = 10.f; |
|
|
|
|
_input_setpoint.y = 10.f; |
|
|
|
|
_input_setpoint.z = -10.f; |
|
|
|
|
|
|
|
|
|
runController(); |
|
|
|
|
EXPECT_EQ(_attitude.thrust_body[0], 0.f); |
|
|
|
@ -198,14 +198,14 @@ TEST_F(PositionControlBasicTest, PositionControlThrustLimit)
@@ -198,14 +198,14 @@ TEST_F(PositionControlBasicTest, PositionControlThrustLimit)
|
|
|
|
|
|
|
|
|
|
TEST_F(PositionControlBasicTest, PositionControlFailsafeInput) |
|
|
|
|
{ |
|
|
|
|
_input_setpoint.vz = 0.7f; |
|
|
|
|
_input_setpoint.acceleration[0] = _input_setpoint.acceleration[1] = 0.0f; |
|
|
|
|
_input_setpoint.vz = .7f; |
|
|
|
|
_input_setpoint.acceleration[0] = _input_setpoint.acceleration[1] = 0.f; |
|
|
|
|
|
|
|
|
|
runController(); |
|
|
|
|
EXPECT_EQ(_attitude.thrust_body[0], 0.f); |
|
|
|
|
EXPECT_EQ(_attitude.thrust_body[1], 0.f); |
|
|
|
|
EXPECT_LT(_output_setpoint.thrust[2], -0.1f); |
|
|
|
|
EXPECT_GT(_output_setpoint.thrust[2], -0.5f); |
|
|
|
|
EXPECT_GT(_attitude.thrust_body[2], -0.5f); |
|
|
|
|
EXPECT_LE(_attitude.thrust_body[2], -0.1f); |
|
|
|
|
EXPECT_LT(_output_setpoint.thrust[2], -.1f); |
|
|
|
|
EXPECT_GT(_output_setpoint.thrust[2], -.5f); |
|
|
|
|
EXPECT_GT(_attitude.thrust_body[2], -.5f); |
|
|
|
|
EXPECT_LE(_attitude.thrust_body[2], -.1f); |
|
|
|
|
} |
|
|
|
|