LIMIT CYCLES IN REACTION JET ATTITUDE CONTROL SYSTEMS SUBJECT TO EXTERNAL TORQUES

Author:

Dahl P.R.,Aldrich G.T.,Herman L.K.

Publisher

Elsevier

Reference14 articles.

1. Stabilization and attitude control of satellite vehicles;Frye;ARS J.,1959

2. Freeman, G.W., “Limit-cycle efficiency of on-off reaction control systems,” Proc. IAS National Specialists Meeting on Guidance of Aerospace Vehicles, Boston, Mass., May 25–27, 1960.

3. Gravitational torque on a satellite vehicle;Roberson;J. Franklin Instit.,1958

4. Roberson, R.E., “Attitude control of a satellite vehicle - an outline of the problems,” in Proc. VIII Congress IAF, Barcelona, 1957, p. 317.

5. Attitude control;DeBra;Elect. Eng.,1958

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. Analysis of jet attitude control systems subject to varying magnitudes of external disturbing torques;Control and Flight Dynamics Conference;1967-08-14

2. A quantized data attitude-control system.;Journal of Spacecraft and Rockets;1966-06

3. The Drag-Free Satellite;AIAA Journal;1964-09

4. Attitude Control in Space a Look at Current Problems and Status;XIIIth International Astronautical Congress Varna 1962 / XIIIe Congrès International D’astronautique / XIII MeждyhapoдhbiЙ ҚohГpecc Пo ActpohabtИқe;1964

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