Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers

Details Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers

Dec 1999

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1999jass...16..265o&link_type=abstract

Journal of Astronomy and Space Sciences, vol. 16, no. 2, p. 265-272.

Astronomy and Astrophysics

Astronomy

Scientific paper

A thrusters modulation method is suggested for spacecraft attitude control with asymmetric configured thrusters during orbit adjustment maneuvers. Attitude is controlled by thrusters off-modulation during orbit maneuvers. Usual control method for symmetric configured thrusters can not be applied for asymmetric configured thrusters. Disturbance induced from thrusters asymmetricity shall be compensated during pulsing. In this paper, a thrusters control method using null solution is suggested, which is shown working well without inducing disturbance.

Affiliated with

Also associated with

No associations

Rating

Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1580027