DEVELOPMENT OF THREE-AXIS DISCRETE MASS ROTATIONAL DYNAMICS MODELS OF FLEXIBLE SPACECRAFT.
Document Type
Conference Proceeding
Publication Date
12-1-1986
Abstract
A three-axis discrete mass model of a flexible spacecraft approximates the rotational dynamics of the vehicle by use of rigid bodies serially connected by a flexible spring-hinge suspension. The equations for this discrete mass model are then developed by applying augmented body methods.
Identifier
0022943033 (Scopus)
ISBN
[087664969X]
Publication Title
Modeling and Simulation Proceedings of the Annual Pittsburgh Conference
First Page
661
Last Page
664
Issue
pt 2
Volume
17
Recommended Citation
Chichester, F. D., "DEVELOPMENT OF THREE-AXIS DISCRETE MASS ROTATIONAL DYNAMICS MODELS OF FLEXIBLE SPACECRAFT." (1986). Faculty Publications. 21025.
https://digitalcommons.njit.edu/fac_pubs/21025
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