Satellite matlab – Examples

Satellite Constellation Access to Ground Station

https://au.mathworks.com/help/satcom/ug/satellite-constellation-access-to-groundstation.html

This is summary note from above link reference: https://au.mathworks.com/help/satcom/ug/satellite-constellation-access-to-groundstation.html

[Images are generated locally in Matlab]

Objective:
The scenario analyzes when a constellation of 40 low-Earth orbit satellites can photograph a specific geographical site located at 42.3001 degrees North and 71.3504 degrees West. Each satellite has an onboard conical sensor (camera) with a 90-degree field of view. The objective is to determine when each satellite can capture images of the site within a six-hour window.

Timeframe:
The analysis takes place on 12 May 2020, from 1:00 PM to 7:00 PM UTC. The simulation uses a sample time of 30 seconds.
Start: 12-May-2020, 1:00 PM UTC
End: 12-May-2020, 7:00 PM UTC
Sample Time: 30 seconds

Access Conditions:
A satellite can photograph the site if two conditions are met:

  1. The site is within the camera’s field of view.
  2. The elevation angle from the satellite to the site is greater than or equal to 30 degrees.

Setup Process:

  • A satellite scenario is created using MATLAB’s satelliteScenario object.
  • Satellites are imported from a TLE file that defines their orbits.
  • A conical sensor (camera) with a 90-degree view angle is attached to each satellite.
  • A ground station is added to represent the geographical site with a minimum elevation angle requirement of 30 degrees.
  • Access analysis is performed between each satellite’s camera and the ground site.
  • The satelliteScenarioViewer is used for visual validation.

System-Wide Access Percentage:
This is the percentage of the total 6-hour period during which at least one satellite can photograph the site. To calculate it:

  • Access status is computed for each satellite.
  • A logical OR operation is applied across all satellites’ access status vectors.
  • The result shows whether at least one satellite has access at each time step.
  • The number of true values is counted and multiplied by the sample time to get total access time.
  • This is divided by the full scenario duration to determine the percentage.

Improvement Through Target Tracking:
Initially, satellites point straight down (nadir), which limits the coverage time due to the fixed field of view. When satellites are made to continuously point at the geographical site using a tracking command, the access intervals improve. This increases the total system-wide access percentage by approximately 36 percent.

Exploration and Adjustments: Various parameters can be modified to influence the results, such as:

  • Changing satellite orbits
  • Adjusting the ground station’s minimum elevation angle
  • Modifying the field of view of the cameras
  • Using gimbals for flexible camera pointing

Conclusion:
This example shows how to evaluate access between a satellite constellation and a ground site using sensors, and how sensor orientation and elevation constraints affect imaging opportunities. It also highlights methods for improving coverage and performance by adjusting satellite and sensor behavior.

Reference:

https://au.mathworks.com/help/satcom/ug/satellite-constellation-access-to-groundstation.html

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