The Control and Use of Drag-free Satellites

Front Cover
Stanford University, 1964 - Artificial satellites - 174 pages

Contents

DERIVATION OF THE DYNAMICAL EQUATIONS
9
SmallAmplitude Linear Motion of a Satellite Including
29
Contactor Translation Control
46
CHAPTER III
70
4
74
Contactor Control of the
81
Contactor Control of the Attitude of the Symmetry Axis of
96
SYSTEM TRAJECTORY ERRORS
109
2
126
CONCLUSION
170
109
173

Bibliographic information

TitleThe Control and Use of Drag-free Satellites
AuthorsBenjamin Otto Lange, Stanford University. Department of Aeronautics and Astronautics
ContributorsStanford University. Department of Electrical Engineering, United States. National Aeronautics and Space Administration
PublisherStanford University, 1964
Length174 pages
  
Export CitationBiBTeX EndNote RefMan