Intelsat IV nutation dynamics-Reference-Cited by-同舟云学术

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Intelsat IV nutation dynamics

Published:1972-04-24 Issue: Volume: Page:
ISSN:
Container-title:4th Communications Satellite Systems Conference
language:
Short-container-title:

Author:

NEER J.¹

Affiliation:

1. Hughes Aircraft Co., Culver City, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1972-537

Reference6 articles.

1. 'Johnson. C. R."TACSAT I Nutation Dynamics. 'I AIAA 3rd Communications Satellite Systems Conference, April 6-8, 1970, Paper No. 70-455. 'Salvatore. J.O., and Bernard, R. H. "Intelsat IV Apogee Boost Study, Report SSD 00061R. Febroary 1970. 310ril 10, A. J. "Analyses Related to the Hughes Gyro.

2. stat System," Hughes Aircraft Company Report SSD 70438B. December 1967.

3. Damping Subsystem Performance, " Hughes IDC 4091.2/005, 9 November 1970.

4. 'Salvatore, J.O., and Porter, W. W. "ATS-VHeat Pipe Tests and Dimensional Analysis, 'I Hughes Aircraft Company Report SGC 10319R, June 1970.

Cited by 2 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. Dual-spin spacecraft stabilization using nutation feedback and inertia coupling;Journal of Spacecraft and Rockets;1976-11

2. Active control of the dynamics of a dual-spin spacecraft;Journal of Spacecraft and Rockets;1975-05

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