SIL Simulink

A software in the loop simulation consists of a Simulink model that simulates the behaviour of the system formed by the autopilot and a vehicle, without having the physical devices connected to the computer, in contrast to the HIL which has both the autopilot and (optionally) vehicle connected to the PC. This option has several advantages when it is compared with a HIL setup:

• Complete simulations without any hardware.

• Possibility of using your own vehicle model: no need to stick to XPlane models. You can add as much physics/complexity as desired.

• Possibility of simulating different kinds of sensors even if they are not fitted in Veronte.

• All results can be exported/visualized to MATLAB workspace simultaneously.

• Veronte Block runs faster than real time, allowing the user to execute a series of simulations in a short time.

• Light computational load.

Autopilot Simulation

The autopilot is implemented in Simulink with an S-Function. This kind of block takes a C, C++, Fortran or even Matlab code, and implements it in a block containing a certain number of inputs and outputs. A typical Veronte s-function is shown below.

S-Function containing the autopilot embedded code

Inputs are described in the next table:

PIN	Signal Type	Description	Form	Size	Units
1	Input	Static Pressure 1	[pressure_measurement;sensor temperature]	2x1	Pa / K
2	Input	Static Pressure 2	[pressure_measurement;sensor temperature]	2x1	Pa / K
3	Input	Static Pressure 3	[pressure_measurement;sensor temperature]	2x1	Pa / K
4	Input	Dynamic Pressure	[pressure_measurement;sensor temperature]	2x1	Pa / K
5	Input	IMU 1	[acc_x;acc_y;acc_z;gyr_x;gyr_y;gyr_z;sensor temperature]	7x1	m/s^2 / m/s / K
6	Input	IMU 2	[acc_x;acc_y;acc_z;gyr_x;gyr_y;gyr_z;sensor temperature]	7x1	m/s^2 / m/s / K
7	Input	IMU 3	[acc_x;acc_y;acc_z;gyr_x;gyr_y;gyr_z;sensor temperature]	7x1	m/s^2 / m/s / K
8	Input	Magnetometer 1	[mag_x;mag_y;mag_z;sensor temperature]	4x1	T
9	Input	Magnetometer 2	[mag_x;mag_y;mag_z;sensor temperature]	4x1	T
10	Input	Magnetometer 3	[mag_x;mag_y;mag_z;sensor temperature]	4x1	T
11	Input	Magnetometer 4	[mag_x;mag_y;mag_z;sensor temperature]	4x1	T
12	Input	GNSS 1	[1;3;lon;lat;alt;hor_accu;vert_accu;v_north;v_east;v_down;v_accu]	11x1	deg *10^7 / mm / mm/s
13	Input	GNSS 2	[1;3;lon;lat;alt;hor_accu;vert_accu;v_north;v_east;v_down;v_accu]	11x1	deg *10^7 / mm / mm/s
14	Input	Relative Position 1	[1;x_rel;y_rel;z_rel;distance_x;distance_y;distance_z;x_accu;y_accu;z_accu]	10x1	cm / mm * 10^-1
15	Input	Relative Position 2	[1;x_rel;y_rel;z_rel;distance_x;distance_y;distance_z;x_accu;y_accu;z_accu]	10x1	cm / mm * 10^-1
16	Input	GPS Time	[week_number;seconds_of_week]	2x1	/ s
17	Input	Lidar 1	[lidar_measurement]	1x1	m
18	Input	Lidar 2	[lidar_measurement]	1x1	m
19	Input	Lidar 3	[lidar_measurement]	1x1	m
20	Input	Lidar 4	[lidar_measurement]	1x1	m
21	Input	Lidar 5	[lidar_measurement]	1x1	m
22	Input	ID Bit Var	[Var_IDs]	50x1	m
23	Input	ID Unsigned Var	[Var_IDs]	50x1	m
24	Input	ID Real Var	[Var_IDs]	50x1	m
25	Input	ADCs	[adc(1-17)]	17x1
26	Input	SCIA Data	[serial_data]	1024x1
27	Input	SCIA Length	[serial_length]	1x1
28	Input	SCIB Data	[serial_data]	1024x1
29	Input	SCIB Length	[serial_length]	1x1
30	Input	SCIC Data	[serial_data]	1024x1
31	Input	SCIC Length	[serial_length]	1x1
32	Input	SCID Data	[serial_data]	1024x1
33	Input	SCID Length	[serial_length]	1x1
34	Input	USB Data	[serial_data]	1024x1
35	Input	USB Length	[serial_length]	1x1

Outputs are the following:

PIN	Signal Type	Description	Form | Size		Units
1	Output	Control Outputs	[control_outputs(1-20)] | 20x1
2	Output	Servo Values	[servos(1-32)]	32x1
3	Output	Position	[lat;lon;alt]	3x1	rad / m
4	Output	Heights	[msl,agl]	2x1	m
5	Output	Velocities	[longitudinal_v;lateral_v;velocity(module)]	3x1	m/s
6	Output	IAS TAS GS	[ias,tas,gs]	3x1	m/s
7	Output	MSL	[msl_from_qnh;msl_from_ISA]	2x1	m
8	Output	Angle of Attack / Sideslip	[angle_of_attack;sideslip]	2x1	rad
9	Output	Q_Infinty	[dynamic_pressure]	1x1	Pa
10	Output	IAS RAW	[ias_raw]	1x1	m/s
11	Output	Tangential Acceleration	[tangential_acceleration]	1x1	m/s^2
12	Input	Body Velocities	[lon_v;lat_v;vertical_v]	3x1	m/s
13	Output	Angular Velocities	[roll_rate;pitch_rate;yaw_rate]	3x1	rad/s
14	Output	Angular Acceleration	[acc_z_axis;acc_y_axis;acc_x_axis]	3x1	rad/^2
15	Output	Acceleration NED	[acc_north;acc_east;acc_down]	3x1	m/s^2
16	Output	Velocity NED	[v_north;v_east;v_down] )	3x1	m/s
17	Output	Angles	[Yaw;Pitch;Roll] )	3x1	rad
18	Output	Co-Angles	[co-Yaw;co-Pitch;co-Roll]	3x1	rad
19	Output	Aerodynamic Angles	[heading,flight_path;bank_angle]	3x1	rad
20	Output	Acceleration Body	[acc_x,acc_y;acc_z]	3x1	m/s^2
21	Output	Load factor	[nx;ny;nz]	3x1
22	Output	SCIA Data	[serial_data]	1024x1
23	Output	SCIA Length	[serial_length]	1x1
24	Output	SCIB Data	[serial_data]	1024x1
25	Output	SCIB Length	[serial_length]	1x1
26	Output	SCIC Data	[serial_data]	1024x1
27	Output	SCIC Length	[serial_length]	1x1
28	Output	SCID Data	[serial_data]	1024x1
29	Output	SCID Length	[serial_length]	1x1
30	Output	USB Data	[serial_data]	1024x1
31	Output	USB Length	[serial_length] )	1x1
32	Output	Unsigned Variables	[selected variables(1-50)]	50x1
33	Output	Bit Variables	[selected variables(1-50)]	50x1
34	Output	Real Variables	[selected variables(1-50)]	50x1

Sensors Simulation & Input Examples

This section aims to ilustrate how to implement the inputs described in the previous section. The structures that are shown here are orientative and, of course, can be adapted by the user.

A basic subsystem that must be built in every flight simulation is an environment model. This model, groups the atmospherical properties and it changes according to different variables as well as the magnetic field at certain coordinates on earth. This block will be the basis of most the sensors that will be shown later on:

Environment Example Block

The static pressure sensor block can be easily derived by taking the pressure from the environment model. The only parameter that must be added is the temperature of the sensor (in this case is the OAT + 60):

Static Pressure Example Block

The dynamic pressure input can be also obtained by using the standard dynamic pressure simulink block. The inputs are the speed (body axis) and the density:

Dynamic Pressure Example Block

There is also a dedicated simulink block in the aerospace blockset that models a set of accelerometers and gyroscopes. The inputs of this block are the acceleration and angular velocities coming out of dynamics of the vehicle.

IMU Example Block

Warning

Do not connect the gravity port to the IMU block.

The magnetometer block is simply a rotated environment magnetic field where the temperature of sensor has been added (same as before OAT + 60). The reason why there is a selector crossing the signals is because there is a rotation matrix pre-configured in each PDI (the real magnetometer is not aligned with the autopilot axis):

Magnetometer Example Block

The GNSS receiver and the relative position input (RTK) are only a multiplexor that creates an array. The position and the velocity are outputs of the vehicle model:

GNSS Receiver Example Block

Relative Position (RTK) Example Block

The analogue inputs follow the same reasoning, the user must add the desired values to the mux:

ADCs Example Block

Veronte can manage input and output serial ports as explained :ref:`here <Device-Others-XPC-Uint8>`_. An easy way to create serial frames (data en length wires) is by using the simulink UDP block. Therefore, the data coming in to veronte should be sent though UDP (if this approach is taken):

SCI Example Block

Monitoring Telemetry with Simulink

As explained before, there are three inputs specially dedicated to select custom telemetry (pins 22,23 and 24). The input structure of those is fixed and must be of size 50, as illustrasted here:

Telemetry ID Mux

The ID of each variable vailable in Veronte can be easily found in Veronte Pipe by adding a new workspace widget. The ID is labelled right before the variable name:

ID indicator

Lastly, to see their values, just place a scope connected to the matching output (pins 32, 33 or 34).

Complete Simulation

After setting the main blocks, the result should look like this:

Complete Setup Example

The main systems are:

• Veronte Autopilot: It contains our flight control software.

• Airframe: a model of the flight dynamics.

• Environment: a model of the atmosphere, magnetic field, WGS84…

• Sensors: it contains individual blocks of all the sensors that veronte needs as input.

• Visualization: It contains, scopes, flight instruments…

The time step should be set to 0.0002 as shown in the next figure in order to guarantee a good GNC/Adquisition frequency:

Time step settings

Connecting Simulink & Veronte Pipe

Our Software-in-the-loop simulator can be connected and used alonside Veronte Pipe software. To do it. Follow this steps:

1. Add a UDP serial communication block and connect it to USB data and length.

2. Add a second UDP serial communication block and connect it to the USB output of veronte.

UDP Blocks

3. Configure your destination port.

Destination UDP Port

4. Set an ethernet network in Preferences as shown using the destination port selected before.

Destination UDP Port (Pipe)

Dealing with PDI files

PDI are uploaded exactly the same way that would be uploaded to a physical autopilot. Once connected to Veronte Pipe, a virtual autopilot will be detected in safe mode, then these steps can be followed.

Warning

Restart functionalities do no restart the simulation and must be done manually.

Veronte S-function deals with a direct copy of the binary files of a veronte autopilot, if a manual setup is needed, these files will be found in the same folder as the simulink block in a subfolder called mmc:

Folder structure (matlab)