Research on the Iteration Guidance Scheme for the Upper Stage of Launch Vehicle in launching Multi-Satellite
- Paper number
IAC-07-D2.I.07
- Author
Mr. Yin ShiMing, Beijing Institute of Astronautical Systems Engineering, China
- Year
2007
- Abstract
To launch and deploy several satellites one time is a very important task for the upper stage of launch vehicle, which need to maneuver between different orbits. This paper studies the iteration guidance scheme with orbit parameters as the constraint conditions directly for lunching multi-satellite. By computing and simulating the trajectory of upper stage for lunching several MEO satellites, it is certified that the guidance scheme is feasible.
- Abstract document