DYNAMIC MODELING FOR EARTH-POINTING SATELLITES TO CONTROL THE THREE-AXIS ATTITUDE WITHOUT THE ATTITUDE INFORMATION OF ONE AXIS

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JAFARBOLAND M.; MOUMENIAN H.R.; SADATI N.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

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Paper Information

Journal: ESTEGHLAL Year:2003 | Volume:21 | Issue:2 Page(s): 1-14

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Information Journal Paper

Title

DYNAMIC MODELING FOR EARTH-POINTING SATELLITES TO CONTROL THE THREE-AXIS ATTITUDE WITHOUT THE ATTITUDE INFORMATION OF ONE AXIS

Author(s)

JAFARBOLAND M. | MOUMENIAN H.R. | SADATI N. | Issue Writer Certificate

Keywords

ATTITUDE CONTROLQ2

PID CONTROLLEYQ2

BIBO STUBILITYQ4

PSEUDO OBSERVERQ4

Abstract

Various methods are presented to control the attitude of satellite due to lack of information of YAW axis attitude so far.In this paper, a new method is used which is more general and is applicable to all types of satellites, with at least one controller. This method is not limited to YAW axis and can control the two other axes as well. One feature of this approach is the ability to be modified for large angle maneuvers for special applications. A new observer is also proposed for the controller, which causes the angle attitude to be kept in desirable values, with minimum control effect and more accuracy. Simulation results show that compare with methods using the complete all axis information, this approach is satisfactory.

Cites

ROBUST TRACKING CONTROL OF SATELLITE ATTITUDE USING NEW EKF FOR LARGE ROTATIONAL MANEUVERS

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APA: Copy

JAFARBOLAND, M., MOUMENIAN, H.R., & SADATI, N.. (2003). DYNAMIC MODELING FOR EARTH-POINTING SATELLITES TO CONTROL THE THREE-AXIS ATTITUDE WITHOUT THE ATTITUDE INFORMATION OF ONE AXIS. ESTEGHLAL, 21(2), 1-14. SID. https://sid.ir/paper/6087/en

Vancouver: Copy

JAFARBOLAND M., MOUMENIAN H.R., SADATI N.. DYNAMIC MODELING FOR EARTH-POINTING SATELLITES TO CONTROL THE THREE-AXIS ATTITUDE WITHOUT THE ATTITUDE INFORMATION OF ONE AXIS. ESTEGHLAL[Internet]. 2003;21(2):1-14. Available from: https://sid.ir/paper/6087/en

IEEE: Copy

M. JAFARBOLAND, H.R. MOUMENIAN, and N. SADATI, “DYNAMIC MODELING FOR EARTH-POINTING SATELLITES TO CONTROL THE THREE-AXIS ATTITUDE WITHOUT THE ATTITUDE INFORMATION OF ONE AXIS,” ESTEGHLAL, vol. 21, no. 2, pp. 1–14, 2003, [Online]. Available: https://sid.ir/paper/6087/en

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