1, determine the initial conditions.
2. Establish the dynamic equation of constellation orbit.
3. Establish a land cover analysis model.
4. Establish the resolution model of Earth observation.
5. The sequential radial basis function multi-objective optimization strategy is adopted to optimize the track height, track inclination and ascending intersection right ascension with coverage and ground pixel resolution as objective functions.
6. Intelligent optimization of satellite constellation is a patented technology applied by Beijing Institute of Technology on 20 17124 October. It is an efficient multi-objective optimization method of satellite constellation and belongs to the field of spacecraft constellation system.