Analysis and verification of a spacecraft wide-angle attitude-control system /
Francis J. Moran and Bruce H. Dishman.

Description

Tools

Cite this Export citation file

Main Author: Moran, Francis J.
Related Names: Dishman, Bruce H.
Ames Research Center.
United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration : 1970.
Subjects: Inertially oriented attitude control.
Euler's theorem.
Physical Description: 44 p. : ill. ; 27 cm.
Locate a Print Version: Find in a library

Viewability

Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign

View HathiTrust MARC record

Similar Items

Experimental investigation of an attitude control system that uses star trackers and inertia wheels

Author: Showman, Robert D.
Published: 1970

The use of a two-degrees-of-freedom gyroscope as a satellite yaw sensor

Author: Moran, Francis J.
Published: 1964

HPCC : NASA

Author: United States. National Aeronautics and Space Administration.
Published: 2000

NASA technical memorandum

Author: United States. National Aeronautics and Space Administration.
Published: 1963

NASA Aviation Safety Reporting System quarterly report number 76-1, April 15, 1976 through July 14, 1976

Author: Ames Research Center.
Published: 1976

Image dissector aperture geometries and scan patterns for use in star tracker systems

Author: Shigemoto, Fred H.
Published: 1965

The highly coupled system : a general approach to the passive attitude stabilization of space vehicles

Author: Merrick, Vernon K.
Published: 1966

NASA technical memorandum

Author: United States. National Aeronautics and Space Administration.
Published: 1959

Analysis of surface ablation of noncharring materials with description of associated computing program

Author: Matting, Fred W.
Published: 1966

The use of integral transforms in the estimation of time variable parameters

Author: Lessing, Henry C.
Published: 1969