Optimal perturbation models for averaged orbit generation
- 16 August 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A recursive formulation for the tesseral disturbing function in equinoctial variablesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- The long-term prediction of artificial satellite orbitsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974