linkIntervals
Description
Examples
Create a satellite scenario object.
startTime = datetime(2020,10,13,7,25,0);
stopTime = startTime + days(1);
sampleTime = 60;                                       % seconds
sc = satelliteScenario(startTime,stopTime,sampleTime);Add a satellite to the scenario.
semiMajorAxis = 10000000; % meters eccentricity = 0; inclination = 10; % degrees rightAscensionOfAscendingNode = 0; % degrees argumentOfPeriapsis = 0; % degrees trueAnomaly = 210; % degrees sat = satellite(sc,semiMajorAxis,eccentricity, ... inclination,rightAscensionOfAscendingNode, ... argumentOfPeriapsis,trueAnomaly);
Add a transmitter to the satellite.
tx = transmitter(sat); pattern(tx);
Add a ground station to the scenario.
latitude = 0; % degrees longitude = 30; % degrees gs = groundStation(sc,latitude,longitude); gb = gimbal(gs);
Add a receiver to the ground station.
rx = receiver(gb); pattern(rx,tx.Frequency);
Create a downlink.
pointAt(gb,sat); pointAt(sat,gs); lnk = link(tx,rx);
Obtain the intervals table of the closed downlink.
intervals = linkIntervals(lnk)
intervals=8×8 table
        Source            Target       IntervalNumber         StartTime                EndTime           Duration    StartOrbit    EndOrbit
    _______________    ____________    ______________    ____________________    ____________________    ________    __________    ________
    "Transmitter 2"    "Receiver 5"          1           13-Oct-2020 07:25:00    13-Oct-2020 07:26:00        60          1            1    
    "Transmitter 2"    "Receiver 5"          2           13-Oct-2020 09:42:00    13-Oct-2020 10:33:00      3060          1            2    
    "Transmitter 2"    "Receiver 5"          3           13-Oct-2020 12:50:00    13-Oct-2020 13:41:00      3060          2            3    
    "Transmitter 2"    "Receiver 5"          4           13-Oct-2020 15:58:00    13-Oct-2020 16:49:00      3060          4            4    
    "Transmitter 2"    "Receiver 5"          5           13-Oct-2020 19:05:00    13-Oct-2020 19:56:00      3060          5            5    
    "Transmitter 2"    "Receiver 5"          6           13-Oct-2020 22:12:00    13-Oct-2020 23:03:00      3060          6            6    
    "Transmitter 2"    "Receiver 5"          7           14-Oct-2020 01:20:00    14-Oct-2020 02:10:00      3000          7            7    
    "Transmitter 2"    "Receiver 5"          8           14-Oct-2020 04:27:00    14-Oct-2020 05:18:00      3060          8            8    
Input Arguments
Link analysis object, specified as a Link object
            vector or scalar.
Output Arguments
Intervals during which the link is closed, returned as a table.
Each row of the table denotes a specific interval, and the columns of the table are
            named as Source, Target,
              IntervalNumber, StartTime,
              EndTime, Duration (in seconds),
              StartOrbit, and EndOrbit.
              Source and Target are the names of the first and
            last node, respectively, which define the link analysis.
- If - Sourceis directly or indirectly attached to a satellite, then- StartOrbitand- EndOrbitcorrespond to the satellite associated with- Source.
- If - Targetis directly or indirectly attached to a satellite, then- StartOrbitand- EndOrbitcorrespond to the satellite associated with- Target. Otherwise,- StartOrbitand- EndOrbitare- NaNbecause they are associated with ground stations.
Note
When the AutoSimulate property of satellite scenario is true, the
        link intervals between StartTime and StopTime are returned. When the property is false, the link
        intervals between StartTime and SimulationTime are returned.
Version History
Introduced in R2021a
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