The present volume is intended both as a report on, and an authoritative reference guide to, the present status of the closely connected fields of Guidance and Control, particularly as related to missiles and space vehicles. Like its predecessor in the series, Volume 8, this volume had its genesis in a Specialist Conference that was held at the Massachusetts Institute of Technology in August 1963. Although in no sense a proceedings of this conference, the present volume uses the same subdivisions of technology, i.e., Attitude Control, Inertial Guidance, Onboard Techniques, Manned Control, Deep Space Guidance and Navigation, Rendezvous, and Landing. To set the stage and to orient those readers who may not have had exposure to the more rapidly growing areas, the Editors have invited certain introductory review articles. They will assist the reader's entry into the subject and into the literature, and in addition they contain information basic to the more complex situations covered in the succeeding papers. In the selection of papers the guiding rule has been the exposure of diverse lines of inquiry, with particular attention given to those current lines of research that appear to be most promising.
Theory of Error Compensation in Astro-Inertial Guidance Systems for Low-Thrust Space Missions
Guidance and Control--II ; 755-774
1964-01-01
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Theory of error compensation in Astro-Inertial-Guidance systems for low-thrust space missions
Engineering Index Backfile | 1964
|Astro inertial navigation systems
Engineering Index Backfile | 1967
|Autonomous navigation and guidance system for low thrust driven deep space missions
British Library Conference Proceedings | 1999
|