Two-dimensional steering of spacecraft, incorporating time shared digital computer, during orbital transfer maneuver, is investigated; effects of sampling and holding, and pulse width modulation on attitude correction maneuver performed in response to prealignment error are studied; amount of additional fuel consumed for entire orbital transfer maneuver due to initial error is shown to be dependent on 4 factors.
Sampled-data velocity vector control of spacecraft
ASME -- Paper
ASME Meeting WA-314 ; 1963 Control
1963
11 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.