Artificial satellite attitude control system

Boots – shoes – and leggings

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

364434, 364453, 244164, 244171, B64G 136, B64G 128

Patent

active

046176349

ABSTRACT:
A system for controlling an attitude of an artificial satellite to decide the present attitude of the satellite on a spatial coordinate and angular velocities of rotation about body axes of the satellite, by the use of inertial sensors and star sensors, to calculate an objective attitude of the satellite on the basis of the present attitude information, the angular velocities of rotation about the body axes and orbit information received from a ground station so that the attitude of the satellite and the changing rate thereof are controlled simultaneously.

REFERENCES:
patent: 3088697 (1963-05-01), Cutler
patent: 3137853 (1964-06-01), Cutler
patent: 3310982 (1967-03-01), Yamron
patent: 3439427 (1969-04-01), Gow
patent: 3866025 (1975-02-01), Cavanagh
patent: 3992106 (1976-11-01), Averbach
patent: 4012018 (1977-03-01), Lorell et al.
patent: 4071211 (1978-01-01), Nahlfelder
patent: 4084773 (1978-04-01), Schmidt, Jr. et al.
patent: 4134681 (1979-01-01), Elmer
patent: 4388646 (1983-06-01), Strother
patent: 4409658 (1983-10-01), Beusse

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Artificial satellite attitude control system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Artificial satellite attitude control system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Artificial satellite attitude control system will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1344036

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.