Guidance and Digital Attitude Control of Mini-satellites and Space Robots ?

摘要

The information mini-satellites (for communication, geodesy, radio- and optoelectronic Earth-observing et al.) and the free-flying space robots (used for servicing both the mini-satellites and manned orbital space stations as well as assembling the large space structures) have some principal problems with respect to their spatial attitude guidance and control. In the paper these problems are considered and obtained results are presented.