Research Article
Guidance Stabilization of Satellites Using the Geomagnetic Field
START; | CALCULATION of ; | FOR TO | CALCULATION of: | – the guide trajectory and the guide stabilizer on ; | – the satellite stabilizer | | using a numerical algorithm to MINIMIZE the in | STEPS, where | , | , | ; | FOR TO | CALCULATION of the satellite trajectory on | | using the stabilizer ; | END | END |
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