Satellite Drag Perturbations in an Oblate Diurnal Atmosphere

Author:

Santora F. A.1

Affiliation:

1. General Electric Company, Valley Forge, Pa.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 16 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Reverse Engineering of Perturbations in the Orbital Decay Environment from Nanosatellite Two-Line Elements;Journal of Spacecraft and Rockets;2022-01

2. Decay of Satellite Orbits Due to the Drag of Rotating Oblate Atmosphere with Scale Height Dependent on Altitude;Arabian Journal for Science and Engineering;2011-02-03

3. Prediction of satellite orbits contraction due to diurnally varying oblate atmosphere and altitude-dependent scale height using KS canonical elements;Planetary and Space Science;2009-09

4. Contraction of satellite orbits using KS uniformly regular canonical elements in an oblate diurnally varying atmosphere;Planetary and Space Science;2007-07

5. Kalman Filter Approach for Re-Eentry Predictions o...;56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law;2005-10-17

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