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논문 기본 정보

자료유형
학술저널
저자정보
Daero Lee (충북대학교) Henry Pernicka (Missouri University of Science & Technology,)
저널정보
한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.12 Number.1
발행연도
2011.3
수록면
43 - 56 (14page)

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초록· 키워드

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An integrated system composed of guidance, navigation and control (GNC) system for autonomous proximity operations and the docking of two spacecraft was developed. The position maneuvers were determined through the integration of the statedependent Riccati equation formulated from nonlinear relative motion dynamics and relative navigation using rendezvous laser vision (Lidar) and a vision sensor system. In the vision sensor system, a switch between sensors was made along the approach phase in order to provide continuously effective navigation. As an extension of the rendezvous laser vision system, an automated terminal guidance scheme based on the Clohessy-Wiltshire state transition matrix was used to formulate a “V-bar hopping approach” reference trajectory. A proximity operations strategy was then adapted from the approach strategy used with the automated transfer vehicle. The attitude maneuvers, determined from a linear quadratic Gaussian-type control including quaternion based attitude estimation using star trackers or a vision sensor system, provided precise attitude control and robustness under uncertainties in the moments of inertia and external disturbances. These functions were then integrated into an autonomous GNC system that can perform proximity operations and meet all conditions for successful docking. A sixdegree of freedom simulation was used to demonstrate the effectiveness of the integrated system.

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Abstract
1. Introduction
2. Overall Proximity Operations Strategy
3. GNC Proximity Operations Architecture
4. Dynamic Modeling
5. Guidance Function
6. Navigation Function
7. Control Function
8. Numerical Results and Analysis
9. Conclusions
Acknowledgments
References

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UCI(KEPA) : I410-ECN-0101-2012-558-004477847