Reliable and Compute Effective Onboard Stationkeeping System for Geostationary Satellites(System Engineerint-III)

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概要

• 論文の詳細を見る

• This paper proposes a new autonomous Stationkeeping system suitable for the geostationary satellites operation and presents the results of the computer simulations conducted to verify the proposed system. The proposed onboard stationkeeping system receives pseudo-range signal from the ground equipments located at two different positions with long baseline, determines the orbit error in real-time and generates orbit control commands. To minimize the complexity of the onboard stationkeeping logic and to achieve the better reliability, a simple orbit controller has been designed which generates a series of control signal making the orbit roughly follow the predetermined reference range data. The reference data are assumed to be generated through ground based computer simulation and onboarded with time tag. Finally, the performance of the proposed system has been verified through the computer simulations.

• 社団法人電子情報通信学会の論文
• 2003-10-17

著者

• Choi Sung-bong

  Communication Satellite Systems Department Kari

• Choi S‐b

  Coms Program Office Korea Aerospace Research Institute

• Choi Seong-bong

  Korea Aerospace Researcg Institute

• PARK Bong-Kyu

  Communication Satellite Systems Department, KARI

• TAHK Min-Jea

  Department of Aerospace Engineering, KAIST

• Park B‐k

  Korea Aerospace Res. Inst. Daejeon Kor

• Tahk Min-jea

  Department Of Aerospace Engineering Kaist

• Park Bong-kyu

  Communication Satellite Systems Department Coms Program Office Korea Aerospace Research Institute

関連論文

• Reliable and Compute Effective Onboard Stationkeeping System for Geostationary Satellites
• Reliable and Compute Effective Onboard Stationkeeping System for Geostationary Satellites(System Engineerint-III)
• Electrical System Design of Prototype Communication Satellite
• Conceptual Design of Communication, Ocean and Meteorological Satellite System
• Conceptual Design of Communication, Ocean and Meteorological Satellite System(System Engineering-II)
• A BUS System Conceptual Design of Experimental Communication Satellite
• Real-Time Orbit Estimation Technique using Input Estimation Filter Algorithm for Geostationary Satellite(System Engineering III)(Joint Conference on Satellite Communications 2004(JC-SAT 2004))
• Biased PNG Law for Impact-Time Control
• Guidance Law for Formation Flight with Terminal Time Constraint

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