In MATLAB's Aerospace Toolbox, the satellite class typically relies on Two-Line Element (TLE) sets to initialize the satellite orbit. As of my knowledge, the toolbox didn't offer a direct method to initialize the satellite using runtime-specified TLE elements without relying on file parsing or compile-time constants. However, you can implement a workaround to achieve your goal. You can create your own class or function that accepts the TLE elements as inputs and initializes the satellite accordingly. Here's a simplified example of how you might do this:
classdef CustomSatellite
properties
TLE; % Store TLE elements
SatelliteObject; % Store the satellite object
end
methods
% Constructor
function obj = CustomSatellite(TLE)
obj.TLE = TLE;
obj.SatelliteObject = satellite(obj.TLE);
end
% Other methods as needed
end
end
Then, you can create an instance of CustomSatellite by passing the TLE elements directly:
% Example TLE elements
TLE = [
'1 25544U 98067A 22068.07910936 .00001269 00000-0 33152-4 0 9997';
'2 25544 51.6450 130.0741 0002884 67.2005 85.3189 15.48857994318422'
];
% Create CustomSatellite object
customSat = CustomSatellite(TLE);
This way, you can pass the TLE elements dynamically at runtime without relying on hardcoded values or file parsing during compilation.
