Aero.trajectory.lissajousTrajectory
R2026bDescription
generates reference signals for a Lissajous trajectory. Lissajous curves are smooth,
continuous patterns obtained from the superposition of orthogonal oscillations. Use
name-value arguments to define the search pattern.refSignals = Aero.trajectory.lissajousTrajectory(Name=Value)
Examples
This example shows how to generate reference signals for a Lissajous trajectory starting at [0,0] meters with a 90-degree initial heading, and ending at [50,50] meters.
refSignals = Aero.trajectory.lissajousTrajectory( ... TrajectoryType="Simple", ... InitialPosition=[0, 0], ... InitialHeading=pi/2, ... FieldCenter=[50, 50], ... Speed=10, ... Altitude=100)
refSignals = struct with fields:
xNorth: [1×1 timeseries]
yEast: [1×1 timeseries]
Speed: [1×1 timeseries]
Altitude: [1×1 timeseries]
Heading: [1×1 timeseries]
FlightPathAngle: [1×1 timeseries]
WaypointIndex: [1×1 timeseries]
LateralAcceleration: [1×1 timeseries]
Name-Value Arguments
Specify optional pairs of arguments as
Name1=Value1,...,NameN=ValueN, where Name is
the argument name and Value is the corresponding value.
Name-value arguments must appear after other arguments, but the order of the
pairs does not matter.
Example: TrajectoryType = "Simple"
Type of Lissajous curve, specified as Simple,
Rectilinear, Circular, or
Star.
Simple— Lissajous curve obtained from superposition of two orthogonal simple harmonic oscillations. TheFrequencyRatioargument determines the shape of the pattern. This curve type sweeps through rectangular regions.Rectilinear— Lissajous curve-like pattern obtained from sawtooth oscillations instead of simple harmonic oscillations. This argument results in straight-line coverage paths with uniform coverage. This curve type sweeps through rectangular regions.Circular— Polar variation of Lissajous curve with orthogonal oscillations along radial and tangential directions. This curve type sweeps through circular sector-like regions.Star— Polar variation of Lissajous curve where the radial coordinate varies along the boundary of an N-pointed star. This curve type sweeps through star-shaped regions.
Example: TrajectoryType = "Circular"
Length of the rectangular field the curve covers, specified as a positive scalar.
Example: FieldLength = 20
Dependencies
To enable this name-value argument, set TrajectoryType to
"Simple" or "Rectilinear".
Data Types: double
Width of the rectangular field the curve covers, specified as a positive scalar.
Example: FieldWidth = 20
Dependencies
To enable this name-value argument, set TrajectoryType to
"Simple" or "Rectilinear".
Data Types: double
Tilt of the field to form a parallelopiped, specified as a scalar in radians in
the range [0, 2*pi].
Example: Tilt = 20*pi/180
Dependencies
To enable this name-value argument, set TrajectoryType to
"Simple" or "Rectilinear".
Data Types: double
Lower and upper bounds on the radius of the circular sector, specified as a 2-element vector.
Example: RadiusRange = [5,20]
Dependencies
To enable this name-value argument, set TrajectoryType to
"Circular".
Data Types: double
Lower and upper bounds on the angular width of the circular sector, specified as a 2-element vector in radians.
Example: AngularRange = [0,pi]
Dependencies
To enable this name-value argument, set TrajectoryType to
"Circular".
Data Types: double
Radius of the circle circumscribing the star-shaped region, specified as a positive scalar.
Example: FieldSize = 50
Dependencies
To enable this name-value argument, set TrajectoryType to
"Star".
Data Types: double
Number of lobes of the star-shaped region, specified as an integer greater than or equal to 2.
Example: NumberOfLobes = 5
Dependencies
To enable this name-value argument, set TrajectoryType to
"Star".
Data Types: double
Shape factor that determines the shape of the star, specified as a scalar in the
range [0, 1]. When Sharpness is
0, the star converges on the circumscribing circle. When
Sharpness is 1, the lobes of the star are
fully distinct.
Example: Sharpness = 0.8
Dependencies
To enable this name-value argument, set TrajectoryType to
"Star".
Data Types: double
Ratio of the oscillation frequencies, specified as a positive scalar. This frequency determines the shape of the Lissajous pattern.
Example: FrequencyRatio = 11/9
Data Types: double
Field center, specified as a 1-by-2 or 2-by-1 vector of finite real doubles in the units specified in Units.
Data Types: double
Bearing, specified as a finite real scalar double between 0 and 2*pi.
Example: Bearing = pi/4
Data Types: double
Starting point of the coverage path within the field, specified as a 2-element vector in radians in the range [0, 2*pi].
Example: InitialPhase = [pi/4,pi/2]
Dependencies
To enable this name-value argument, set TrajectoryType to
Simple or Circular.
Data Types: double
Number of cycles for which the Lissajous curve is generated, specified as a positive scalar.
Example: Cycles = 2
Data Types: double
Number of samples in the output signals, specified as a scalar greater than or equal to 2.
Example: NumberOfSamples = 10
Data Types: double
Initial position of trajectory, specified as a 1-by-2 or 2-by-1 vector in the units specified in Units.
Example: InitialPosition = [0,0]
Data Types: double
Speed of trajectory, specified as a finite real double scalar in the units specified in Units.
Example: Speed = 10
Data Types: double
Initial altitude of trajectory, specified as a scalar in the units specified in Units.
Example: InitialAltitude = 10
Data Types: double
Initial heading of trajectory, specified as a real scalar between 0 and
2*pi, in radians. Specify at least one or both
InitialHeading and FinalHeading.
Example: InitialHeading = pi
Data Types: double
Type of reference signal, specified as None,
lateral-acceleration, or
turnrate.
Example:
ReferenceSignalType = "turnrate"
Output format of reference signals data, specified as a timeseries
or timetable object.
Example: OutputFormat = timeseries
Input and output units, specified as one of these values.
Units | Position | Altitude | Speed |
|---|---|---|---|
| Meters | Meters | Meters per second |
| Feet | Feet | Feet per second |
| Nautical miles | Feet | Knots |
Example: Units = 'Metric (MKS)'
Initial time of trajectory operation, specified as a datetime object.
Example: StartTime = datetime('now')
Prior trajectory tracking data, specified as a timeseries or
timetable object. These objects must contain these fields:
AltitudeHeadingSpeedWaypointIndexxNorthyEastLateralAcceleraion/Turnrate
Output Arguments
Trajectory reference signals, returned as a timeseries
struct or timetable object.
Version History
Introduced in R2026b
See Also
Live Editor Tasks
Functions
Aero.trajectory.addEvent|Aero.trajectory.bezierTrajectory|Aero.trajectory.circularTrajectory|Aero.trajectory.creepingTrajectory|Aero.trajectory.expandingSquareTrajectory|Aero.trajectory.merge|Aero.trajectory.parallelSweepTrajectory|Aero.trajectory.polylineTrajectory|Aero.trajectory.polynomialTrajectory|Aero.trajectory.sectorTrajectory|Aero.trajectory.spaceFillingTrajectory|Aero.trajectory.tracklineTrajectory
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