Analysis of the influences of different parameters on a reaction jet single-axis satellite attitude control system /
Hans-Paul Riemann.

Description

Main Author

Riemann, Hans-Paul.

Related Names

Air Force Flight Dynamics Laboratory (U.S.)

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965.

Subjects

Artificial satellites > Artificial satellites / Attitude control systems.
Space vehicles > Space vehicles / Attitude control systems.

Note

"August 1965."

Physical Description

vii, 22 pages : illustrations ; 28 cm.

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