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Accession Number ADA601088
Title Attitude Dynamics/Control of Dual-Body Spacecraft with Variable-Speed Control Moment Gyros.
Publication Date Jul 2004
Media Count 14p
Personal Author B. N. Agrawal M. Romano
Abstract The dynamics equations of a spacecraft consisting of two bodies mutually rotating around a common gimbal axis are derived by the use of the Newton Euler approach. One of the bodies contains a cluster of single-gimbal variable-speed control moment gyros. T ...
Keywords Attitude control systems
Newton-euler methods
Numerical analysis
Variable speed drives

Source Agency Non Paid ADAS
NTIS Subject Category 51E - Avionics
41J - Tooling, Machinery, & Tools
76D - Navigation Systems
84G - Unmanned Spacecraft
Corporate Author Naval Postgraduate School, Monterey, CA.
Document Type Journal article
Title Note Journal article.
NTIS Issue Number 1421
Contract Number N/A

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