Attitude determination and control subsystem for the TOPEX satellite-Reference-Cited by-同舟云学术

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Attitude determination and control subsystem for the TOPEX satellite

Published:1988-08-15 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation and Control Conference
language:
Short-container-title:

Author:

DENNEHY C.¹,WELCH R.¹,KIA T.²

Affiliation:

1. Fairchild Space Co., Germantown, MD

2. California Institute of Technology, Jet Propulsion Laboratory,Pasadena

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-4129

Reference12 articles.

1. Stewart,R.A.,and M. Lefebvre,"TOPEX/POSEIDON: A Contribution to the World Climate Research Program," AAS Paper 86-306

2. MultimissionModular SpacecraftExternal InterfaceSpecification and User's Guide, NASA/GSFC Document S700-11, February 1978

3. Das, A. "The On-Orbit Attitude Determination and Control Systemfor the LANDSAT-D Spacecraft," AIAA Paper 82-310

Cited by 4 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. Quality assessment of the nominal attitude model of TOPEX/Poseidon using quaternion data;Advances in Space Research;2024-06

2. Advanced X-ray Astrophysics Facility-Spectrometry Spacecraft Pointing Control System - Conceptual design;Journal of Spacecraft and Rockets;1995-03

3. Conceptual design of the pointing control system for AXAF-S;Space Programs and Technologies Conference and Exhibit;1993-08-22

4. Optimal temperature estimation for modeling the thermal elastic shock disturbance torque;Journal of Spacecraft and Rockets;1991-07

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