Relationship is derived for drift of coordinate transformation matrix of quantized (pulsed) attitude reference system on vehicle undergoing "coning motion"; several sources of limit cycle oscillations in missiles and spacecraft are studied to determine nature of such coning motions; typical transformation drifts are computed for these system effects.
Drift of quantized attitude system due to vehicle coning motions
SAE-NASA -- Proc
Proceedings of the SAE-NASA -- Aerospace Vehicle Flight Control Conference ; 1965 Control
1965
4 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
The Drift of a Quantized Attitude System Due to Vehicle Coning Motions
SAE Technical Papers | 1965
|Attitude reorientation of spacecraft by means of impulse coning
TIBKAT | 1977
|