Attitude Control by Asymmetric Thrusters' Independent off Modulation during Orbit Adjustment Maneuvers
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...
Main Author: | Hwa-Suk Oh |
---|---|
Format: | Article |
Language: | English |
Published: |
Korean Space Science Society (KSSS)
1999-12-01
|
Series: | Journal of Astronomy and Space Sciences |
Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1999/v16n2/OJOOBS_1999_v16n2_265.pdf |
Similar Items
-
Experiments and numerical simulations of the dynamics of an R.O.V. thruster during maneuvering
by: Knowles, James H. (James Hugh)
Published: (2007) -
Minimum vibration maneuvers using input shaping and pulse-width, pulse frequency modulated thruster control
by: Buck, Nicholas V.
Published: (2013) -
A comparative study of various approaches to the design of on-off thruster attitude control systems
by: Weisenberg, David Marc
Published: (2005) -
Orbital Dynamics of a Simple Solar Photon Thruster
by: Anna D. Guerman, et al.
Published: (2009-01-01) -
Uncertainty Requirement Analysis for the Orbit, Attitude, and Burn Performance of the 1st Lunar Orbit Insertion Maneuver
by: Young-Joo Song, et al.
Published: (2016-12-01)