New Approach to Mission Design Based on the Fundamental Equations of Motion-Reference-Cited by-同舟云学术

New Approach to Mission Design Based on the Fundamental Equations of Motion

Published:2006-04 Issue:2 Volume:19 Page:59-67
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lam Try¹

Affiliation:

1. Member of the Engineering Staff, Guidance, Navigation, and Control Section, Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Dr., Pasadena, CA 91109.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282006%2919%3A2%2859%29

Reference20 articles.

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2. Inclination of satellite orbits about an oblate precessing planet

3. Hussein I. I. and Scheeres D. J. (2004). “Effects of orbit perturbations on a class of earth-orbiting interferometric observatories.” Proc. Spaceflight Mechanics Meeting Maui Hawaii AAS Paper 2004-210.

4. Low thrust OTV guidance using Lyapunov optimal feedback control techniques;Ilgen M. R.;Adv. Astronaut. Sci.,1993

5. The motion of a close earth satellite

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