Semipassive and active nutation dampers for dual-spin spacecraft-Reference-Cited by-同舟云学术

Semipassive and active nutation dampers for dual-spin spacecraft

Published:1971-05 Issue:5 Volume:8 Page:448-455
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

MINGORI D. L.¹,HARRISON J. A.¹,TSENG G. T.¹

Affiliation:

1. University of California, Los Angeles, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.30300

Reference8 articles.

1. Nutational stability of an axisymmetric body containing a rotor

2. Attitude stability criteria for dual spin spacecraft.

3. Effects of energy dissipation on the attitude stability of dual-spinsatellites.

4. Proceedings of the Symposium on Attitude Stabilization and Control of Dual-Spin Spacecraft, TR 0158(3307-01)-16,Nov. 1967, Aerospace Corp., El Segundo, Calif., pp.73-109; also Rept. SAMSO-TR-68-191, U.S. Air Force.

Cited by 6 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. High precision active nutation control of a momentum biased spacecraft with flexible appendages;Journal of Guidance, Control, and Dynamics;1985-01

2. Dual-spin satellites with gyro-damping;Acta Astronautica;1982-05

3. A Semi-Active Nutation Damper for Spinning Prolate or Oblate Satellites;IFAC Proceedings Volumes;1976-05

4. Active stabilization of a dual-spin spacecraft using imbalance;Journal of Spacecraft and Rockets;1975-12

5. Design and ground test of a pendulum-type active nutation damper;Journal of Spacecraft and Rockets;1974-11