Dynamics of a spinning space station with a counterweight connected by multiple cables

Author:

NIXON D.1

Affiliation:

1. NASA, Marshall Space Flight Center, Aero-Astrodynamics Laboratory, Huntsville, Ala.

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Equations (45) and (47) represent the (1,1) and (3,3) elements (3 x 3's) of 'vJ, nnd are in a form which can be readily programmed on a digital computer. P; kand Q.;1, have particulai: exp1.·essions associated with each set of subscript values which are obtained directly by taking rivatives of t-he elements of A and 8 with respect to the various Euler ,mg les in accord,mce with the definitions of Pc; It and Q;_i k . These cxpressi ons were derived for a l, 2, 3 Euler rotation sequence and wei:e programmed to be evaluatE'd ns necessary. Since the (2,2) element (3 x 3) of 'v'c1is expressed in final form in equation (36), and all of the other clerncnts arc zero, the

2. 0 .10 "'"'"t-r"T'4-

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. Dynamics of a tethered satellite with variable mass;Discrete & Continuous Dynamical Systems - S;2015

2. A Movable-Mass Attitude Stabilization System For Cable-Connected Artificial-^ Space Stations;Journal of Spacecraft and Rockets;1974-03

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