Spacecraft Design Project Low Earth Orbit Communications Satellite
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This report is the final product of the spacecraft design project completed to fulfill the academic requirements of the Spacecraft Design and Integration II course (AE-4871) taught at the U.S. Naval Postgraduate School.
NASA-CR-192038AE-4871 Advance Spacecraft Design
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Agrawal, B.N. (2005);This paper presents a review of the spacecraft design program at the Naval Postgraduate School. This program is part of the space systems engineering curriculum. In this curriculum, the students take at least one course ...
Romano, M.; Agrawal, B. (2004);The dynamics equations of a spacecraft consisting of two bodies mutually rotating around a common gimbal axis are derived by the use of the Newton–Euler approach. One of the bodies contains a cluster of single-gimbal var ...
Bang, H.; Agrawal, B.N. (1994);A new approach for spacecraft maneuver based upon constraint dynamics and tracking control laws is presented in this paper. For high precision pointing requirement on spacecraft maneuver, a desired trajectory is prescribed ...