Techniques proposed to compensate guidance errors in aided-inertial guidance systems for long-term, low-thrust space missions are rotation of accelerometers with respect to inertially stabilized platform, statistical filtering of redundant position and/or velocity information and output of inertially fixed accelerometers, and combination of statistical filtering and rotation of accelerometers; effectiveness of techniques is analyzed; analytical and numerical results.
Theory of error compensation in Astro-Inertial-Guidance systems for low-thrust space missions
Progress Astronautics Aeronautics
1964
20 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Error propagation in astro-inertial guidance systems for low-thrust missions
Engineering Index Backfile | 1964
|Astro inertial navigation systems
Engineering Index Backfile | 1967
|