The Drift of a Quantized Attitude System Due to Vehicle Coning Motions Kearfott-San Marcos, Div. of General Precision, Incorporated

Format:

Conference/Event

Author/Creator:

Schmitt, A. F., author.

Conference Name:

NASA Aerospace Vehicle Flight Control Conference (1965-07-13 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1965

Summary:

A relationship is derived for the drift of a coordinate transformation matrix of a quantized (pulsed) attitude reference system on a vehicle undergoing a "coning motion". Several sources of limit cycle oscillations in missiles and spacecraft are studied to determine the nature of such coning motions. Typical transformation drifts are computed for these system effects

Notes:

Vendor supplied data

Publisher Number:

650587

Access Restriction:

Restricted for use by site license