Documents in the NTIS Technical Reports collection are the results of federally funded research. They are directly submitted to or collected by NTIS from Federal agencies for permanent accessibility to industry, academia and the public.  Before purchasing from NTIS, you may want to check for free access from (1) the issuing organization's website; (2) the U.S. Government Printing Office's Federal Digital System website http://www.gpo.gov/fdsys; (3) the federal government Internet portal USA.gov; or (4) a web search conducted using a commercial search engine such as http://www.google.com.
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
Dynamics
Equations
Gyroscopes
Inertia
Newton-euler methods
Numerical analysis
Rotation
Spacecraft
Telescopes
Tracking
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

Science and Technology Highlights

See a sampling of the latest scientific, technical and engineering information from NTIS in the NTIS Technical Reports Newsletter

Acrobat Reader Mobile    Acrobat Reader