# insSensor

Inertial navigation system and GNSS/GPS simulation model

## Description

The `insSensor`

System object™ models a device that fuses measurements from an inertial navigation system (INS)
and global navigation satellite system (GNSS) such as a GPS, and outputs the fused
measurements.

To output fused INS and GNSS measurements:

Create the

`insSensor`

object and set its properties.Call the object with arguments, as if it were a function.

To learn more about how System objects work, see What Are System Objects?

## Creation

### Description

returns a System object, `INS`

= insSensor`INS`

, that models a device that outputs measurements from
an INS and GNSS.

sets properties using one or
more name-value pairs. Unspecified properties have default values. Enclose each property
name in quotes.`INS`

= insSensor(`Name,Value`

)

## Properties

Unless otherwise indicated, properties are *nontunable*, which means you cannot change their
values after calling the object. Objects lock when you call them, and the
`release`

function unlocks them.

If a property is *tunable*, you can change its value at
any time.

For more information on changing property values, see System Design in MATLAB Using System Objects.

`MountingLocation`

— Location of sensor on platform (m)

`[0 0 0]`

(default) | three-element real-valued vector of form [*x*
*y*
*z*]

Location of the sensor on the platform, in meters, specified as a three-element
real-valued vector of the form [*x*
*y*
*z*]. The vector defines the offset of the sensor origin from the
origin of the platform.

**Tunable: **Yes

**Data Types: **`single`

| `double`

`RollAccuracy`

— Accuracy of roll measurement (deg)

`0.2`

(default) | nonnegative real scalar

Accuracy of the roll measurement of the sensor body, in degrees, specified as a nonnegative real scalar.

*Roll* is the rotation around the *x*-axis of
the sensor body. Roll noise is modeled as a white noise process.
`RollAccuracy`

sets the standard deviation of the roll measurement
noise.

**Tunable: **Yes

**Data Types: **`single`

| `double`

`PitchAccuracy`

— Accuracy of pitch measurement (deg)

`0.2`

(default) | nonnegative real scalar

Accuracy of the pitch measurement of the sensor body, in degrees, specified as a nonnegative real scalar.

*Pitch* is the rotation around the *y*-axis of
the sensor body. Pitch noise is modeled as a white noise process.
`PitchAccuracy`

defines the standard deviation of the pitch
measurement noise.

**Tunable: **Yes

**Data Types: **`single`

| `double`

`YawAccuracy`

— Accuracy of yaw measurement (deg)

`1`

(default) | nonnegative real scalar

Accuracy of the yaw measurement of the sensor body, in degrees, specified as a nonnegative real scalar.

*Yaw* is the rotation around the *z*-axis of
the sensor body. Yaw noise is modeled as a white noise process.
`YawAccuracy`

defines the standard deviation of the yaw measurement
noise.

**Tunable: **Yes

**Data Types: **`single`

| `double`

`PositionAccuracy`

— Accuracy of position measurement (m)

`[1 1 1]`

(default) | nonnegative real scalar | three-element real-valued vector

Accuracy of the position measurement of the sensor body, in meters, specified as a
nonnegative real scalar or a three-element real-valued vector. The elements of the
vector set the accuracy of the *x*-, *y*-, and
*z*-position measurements, respectively. If you specify
`PositionAccuracy`

as a scalar value, then the object sets the
accuracy of all three positions to this value.

Position noise is modeled as a white noise process.
`PositionAccuracy`

defines the standard deviation of the position
measurement noise.

**Tunable: **Yes

**Data Types: **`single`

| `double`

`VelocityAccuracy`

— Accuracy of velocity measurement (m/s)

`0.05`

(default) | nonnegative real scalar

Accuracy of the velocity measurement of the sensor body, in meters per second, specified as a nonnegative real scalar.

Velocity noise is modeled as a white noise process.
`VelocityAccuracy`

defines the standard deviation of the velocity
measurement noise.

**Tunable: **Yes

**Data Types: **`single`

| `double`

`AccelerationAccuracy`

— Accuracy of acceleration measurement (m/s^{2})

`0`

(default) | nonnegative real scalar

Accuracy of the acceleration measurement of the sensor body, in meters per second, specified as a nonnegative real scalar.

Acceleration noise is modeled as a white noise process.
`AccelerationAccuracy`

defines the standard deviation of the
acceleration measurement noise.

**Tunable: **Yes

**Data Types: **`single`

| `double`

`AngularVelocityAccuracy`

— Accuracy of angular velocity measurement (deg/s)

`0`

(default) | nonnegative real scalar

Accuracy of the angular velocity measurement of the sensor body, in meters per second, specified as a nonnegative real scalar.

Angular velocity is modeled as a white noise process.
`AngularVelocityAccuracy`

defines the standard deviation of the
acceleration measurement noise.

**Tunable: **Yes

**Data Types: **`single`

| `double`

`TimeInput`

— Enable input of simulation time

`false`

or `0`

(default) | `true`

or `1`

Enable input of simulation time, specified as a logical `0`

(`false`

) or `1`

(`true`

). Set this
property to `true`

to input the simulation time by using the `simTime`

argument.

**Tunable: **No

**Data Types: **`logical`

`HasGNSSFix`

— Enable GNSS fix

`true`

or `1`

(default) | `false`

or `0`

Enable GNSS fix, specified as a logical `1`

(`true`

) or `0`

(`false`

). Set this
property to `false`

to simulate the loss of a GNSS receiver fix. When a
GNSS receiver fix is lost, position measurements drift at a rate specified by the
`PositionErrorFactor`

property.

**Tunable: **Yes

#### Dependencies

To enable this property, set `TimeInput`

to
`true`

.

**Data Types: **`logical`

` PositionErrorFactor`

— Position error factor without GNSS fix

`[0 0 0]`

(default) | nonnegative scalar | 1-by-3 vector of scalars

Position error factor without GNSS fix, specified as a scalar or a 1-by-3 vector of scalars.

When the `HasGNSSFix`

property is set to
`false`

, the position error grows at a quadratic rate due to constant
bias in the accelerometer. The position error for a position component
*E*(*t*) can be expressed as
*E*(*t*) =
1/2*α**t*^{2}, where
*α* is the position error factor for the corresponding component and
*t* is the time since the GNSS fix is lost. While running, the object
computes *t* based on the `simTime`

input. The
computed *E*(*t*) values for the *x*,
*y*, and *z* components are added to the
corresponding position components of the `gTruth`

input.

**Tunable: **Yes

#### Dependencies

To enable this property, set `TimeInput`

to
`true`

and `HasGNSSFix`

to
`false`

.

**Data Types: **`single`

| `double`

`RandomStream`

— Random number source

`'Global stream'`

(default) | `'mt19937ar with seed'`

Random number source, specified as one of these options:

`'Global stream'`

–– Generate random numbers using the current global random number stream.`'mt19937ar with seed'`

–– Generate random numbers using the mt19937ar algorithm, with the seed specified by the`Seed`

property.

**Data Types: **`char`

| `string`

`Seed`

— Initial seed

`67`

(default) | nonnegative integer

Initial seed of the mt19937ar random number generator algorithm, specified as a nonnegative integer.

#### Dependencies

To enable this property, set `RandomStream`

to
`'mt19937ar with seed'`

.

**Data Types: **`single`

| `double`

| `int8`

| `int16`

| `int32`

| `int64`

| `uint8`

| `uint16`

| `uint32`

| `uint64`

## Usage

### Description

models the data received from an INS sensor reading and GNSS sensor reading. The output
measurement is based on the inertial ground-truth state of the sensor body,
`measurement`

= INS(`gTruth`

)`gTruth`

.

additionally specifies the time of simulation, `measurement`

= INS(`gTruth`

,`simTime`

)`simTime`

. To enable
this syntax, set the `TimeInput`

property to `true`

.

### Input Arguments

`gTruth`

— Inertial ground-truth state of sensor body

structure

Inertial ground-truth state of sensor body, in local Cartesian coordinates, specified as a structure containing these fields:

Field | Description |
---|---|

`'Position'` | Position, in meters, specified as a real, finite |

`'Velocity'` | Velocity ( |

`'Orientation'` | Orientation with respect to the local Cartesian coordinate system, specified as one of these options: *N*-element column vector of`quaternion` objects3-by-3-by- *N*array of rotation matrices*N*-by-3 matrix of [*x*_{roll}*y*_{pitch}*z*_{yaw}] angles in degrees
Each quaternion or rotation matrix is a frame rotation from
the local Cartesian coordinate system to the current sensor body coordinate
system. |

`'Acceleration'` | Acceleration ( |

`'AngularVelocity'` | Angular velocity ( |

The field values must be of type `double`

or
`single`

.

The `Position`

, `Velocity`

, and
`Orientation`

fields are required. The other fields are
optional.

**Example: **```
struct('Position',[0 0 0],'Velocity',[0 0
0],'Orientation',quaternion([1 0 0 0]))
```

`simTime`

— Simulation time

nonnegative real scalar

Simulation time, in seconds, specified as a nonnegative real scalar.

**Data Types: **`single`

| `double`

### Output Arguments

`measurement`

— Measurement of sensor body motion

structure

Measurement of the sensor body motion, in local Cartesian coordinates, returned as a structure containing these fields:

Field | Description |
---|---|

`'Position'` | Position, in meters, specified as a real, finite |

`'Velocity'` | Velocity ( |

`'Orientation'` | Orientation with respect to the local Cartesian coordinate system, specified as one of these options: *N*-element column vector of`quaternion` objects3-by-3-by- *N*array of rotation matrices*N*-by-3 matrix of [*x*_{roll}*y*_{pitch}*z*_{yaw}] angles in degrees
Each quaternion or rotation matrix is a frame rotation from
the local Cartesian coordinate system to the current sensor body coordinate
system. |

`'Acceleration'` | Acceleration ( |

`'AngularVelocity'` | Angular velocity ( |

The returned field values are of type `double`

or
`single`

and are of the same type as the corresponding field values
in the `gTruth`

input.

## Object Functions

To use an object function, specify the
System object as the first input argument. For
example, to release system resources of a System object named `obj`

, use
this syntax:

release(obj)

### Specific to `insSensor`

`perturbations` | Perturbation defined on object |

`perturb` | Apply perturbations to object |

## Examples

### Generate INS Measurements from Stationary Input

Create a motion structure that defines a stationary position at the local north-east-down (NED) origin. Because the platform is stationary, you need to define only a single sample. Assume the ground-truth motion is sampled for 10 seconds with a 100 Hz sample rate. Create a default `insSensor`

System object™. Preallocate variables to hold output from the `insSensor`

object.

Fs = 100; duration = 10; numSamples = Fs*duration; motion = struct( ... 'Position',zeros(1,3), ... 'Velocity',zeros(1,3), ... 'Orientation',ones(1,1,'quaternion')); INS = insSensor; positionMeasurements = zeros(numSamples,3); velocityMeasurements = zeros(numSamples,3); orientationMeasurements = zeros(numSamples,1,'quaternion');

In a loop, call `INS`

with the stationary motion structure to return the position, velocity, and orientation measurements in the local NED coordinate system. Log the position, velocity, and orientation measurements.

for i = 1:numSamples measurements = INS(motion); positionMeasurements(i,:) = measurements.Position; velocityMeasurements(i,:) = measurements.Velocity; orientationMeasurements(i) = measurements.Orientation; end

Convert the orientation from quaternions to Euler angles for visualization purposes. Plot the position, velocity, and orientation measurements over time.

orientationMeasurements = eulerd(orientationMeasurements,'ZYX','frame'); t = (0:(numSamples-1))/Fs; subplot(3,1,1) plot(t,positionMeasurements) title('Position') xlabel('Time (s)') ylabel('Position (m)') legend('North','East','Down') subplot(3,1,2) plot(t,velocityMeasurements) title('Velocity') xlabel('Time (s)') ylabel('Velocity (m/s)') legend('North','East','Down') subplot(3,1,3) plot(t,orientationMeasurements) title('Orientation') xlabel('Time (s)') ylabel('Rotation (degrees)') legend('Roll', 'Pitch', 'Yaw')

### Generate INS Measurements from Driving Scenario

Generate measurements from an INS sensor that is mounted to a vehicle in a driving scenario. Plot the INS measurements against the ground truth state of the vehicle and visualize the velocity and acceleration profile of the vehicle.

**Create Driving Scenario**

Load the geographic data for a driving route at the MathWorks® Apple Hill campus in Natick, MA.

```
data = load('ahroute.mat');
latIn = data.latitude;
lonIn = data.longitude;
```

Convert the latitude and longitude coordinates of the route to Cartesian coordinates. Set the origin to the first coordinate in the driving route. For simplicity, assume an altitude of 0 for the route.

alt = 0; origin = [latIn(1),lonIn(1),alt]; [xEast,yNorth,zUp] = latlon2local(latIn,lonIn,alt,origin);

Create a driving scenario. Set the origin of the converted route as the geographic reference point.

```
scenario = drivingScenario('GeoReference',origin);
```

Create a road based on the Cartesian coordinates of the route.

roadCenters = [xEast,yNorth,zUp]; road(scenario,roadCenters);

Create a vehicle that follows the center line of the road. The vehicle travels between 4 and 5 meters per second (9 to 11 miles per hour), slowing down at the curves in the road. To create the trajectory, use the `smoothTrajectory`

function. The computed trajectory minimizes jerk and avoids discontinuities in acceleration, which is a requirement for modeling INS sensors.

```
egoVehicle = vehicle(scenario,'ClassID',1);
egoPath = roadCenters;
egoSpeed = [5 5 5 4 4 4 5 4 4 4 4 5 5 5 5 5];
smoothTrajectory(egoVehicle,egoPath,egoSpeed);
```

Plot the scenario and show a 3-D view from behind the ego vehicle.

plot(scenario) chasePlot(egoVehicle)

**Create INS Sensor**

Create an INS sensor that accepts the input of simulation times. Introduce noise into the sensor measurements by setting the standard deviation of velocity and accuracy measurements to 0.1 and 0.05, respectively.

INS = insSensor('TimeInput',true, ... 'VelocityAccuracy',0.1, ... 'AccelerationAccuracy',0.05);

**Visualize INS Measurements**

Initialize a geographic player for displaying the INS measurements and the actor ground truth. Configure the player to display its last 10 positions and set the zoom level to 17.

zoomLevel = 17; player = geoplayer(latIn(1),lonIn(1),zoomLevel, ... 'HistoryDepth',10,'HistoryStyle','line');

Pre-allocate space for the simulation times, velocity measurements, and acceleration measurements that are captured during simulation.

numWaypoints = length(latIn); times = zeros(numWaypoints,1); gTruthVelocities = zeros(numWaypoints,1); gTruthAccelerations = zeros(numWaypoints,1); sensorVelocities = zeros(numWaypoints,1); sensorAccelerations = zeros(numWaypoints,1);

Simulate the scenario. During the simulation loop, obtain the ground truth state of the ego vehicle and an INS measurement of that state. Convert these readings to geographic coordinates, and at each waypoint, visualize the ground truth and INS readings on the geographic player. Also capture the velocity and acceleration data for plotting the velocity and acceleration profiles.

nextWaypoint = 2; while advance(scenario) % Obtain ground truth state of ego vehicle. gTruth = state(egoVehicle); % Obtain INS sensor measurement. measurement = INS(gTruth,scenario.SimulationTime); % Convert readings to geographic coordinates. [latOut,lonOut] = local2latlon(measurement.Position(1), ... measurement.Position(2), ... measurement.Position(3),origin); % Plot differences between ground truth locations and locations reported by sensor. reachedWaypoint = sum(abs(roadCenters(nextWaypoint,:) - gTruth.Position)) < 1; if reachedWaypoint plotPosition(player,latIn(nextWaypoint),lonIn(nextWaypoint),'TrackID',1) plotPosition(player,latOut,lonOut,'TrackID',2,'Label','INS') % Capture simulation times, velocities, and accelerations. times(nextWaypoint,1) = scenario.SimulationTime; gTruthVelocities(nextWaypoint,1) = gTruth.Velocity(2); gTruthAccelerations(nextWaypoint,1) = gTruth.Acceleration(2); sensorVelocities(nextWaypoint,1) = measurement.Velocity(2); sensorAccelerations(nextWaypoint,1) = measurement.Acceleration(2); nextWaypoint = nextWaypoint + 1; end if nextWaypoint > numWaypoints break end end

**Plot Velocity Profile**

Compare the ground truth longitudinal velocity of the vehicle over time against the velocity measurements captured by the INS sensor.

Remove zeros from the time vector and velocity vectors.

times(times == 0) = []; gTruthVelocities(gTruthVelocities == 0) = []; sensorVelocities(sensorVelocities == 0) = []; figure hold on plot(times,gTruthVelocities) plot(times,sensorVelocities) title('Longitudinal Velocity Profile') xlabel('Time (s)') ylabel('Velocity (m/s)') legend('Ground truth','INS') hold off

**Plot Acceleration Profile**

Compare the ground truth longitudinal acceleration of the vehicle over time against the acceleration measurements captured by the INS sensor.

gTruthAccelerations(gTruthAccelerations == 0) = []; sensorAccelerations(sensorAccelerations == 0) = []; figure hold on plot(times,gTruthAccelerations) plot(times,sensorAccelerations) title('Longitudinal Acceleration Profile') xlabel('Time (s)') ylabel('Acceleration (m/s^2)') legend('Ground truth','INS') hold off

## Tips

To obtain the ground-truth state of actors in a driving scenario, use the

`state`

function.The sensor reports measurements in the local Cartesian coordinate system. To convert these measurements to geographic positions for visualization on a map, use the

`local2latlon`

function. To convert this data back to local coordinates, use the`latlon2local`

function.

## Extended Capabilities

### C/C++ Code Generation

Generate C and C++ code using MATLAB® Coder™.

The object functions, `perturbations`

and
`perturb`

, do not support code generation.

Usage notes and limitations:

See System Objects in MATLAB Code Generation (MATLAB Coder).

## Version History

**Introduced in R2021a**

## See Also

### Objects

### Objects

## MATLAB 명령

다음 MATLAB 명령에 해당하는 링크를 클릭했습니다.

명령을 실행하려면 MATLAB 명령 창에 입력하십시오. 웹 브라우저는 MATLAB 명령을 지원하지 않습니다.

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