지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.18 Number.2
- 발행연도
- 2017.6
- 수록면
- 300 - 314 (15page)
- DOI
- 10.5139/IJASS.2017.18.2.300
이용수
초록· 키워드
오류제보하기
This paper examines finite rotation angle (FRA) applications for spacecraft attitude control. The coordinate transformation matrix and the attitude kinematics represented by FRAs are introduced. The interpolation techniques for the angular orientations are thoroughly investigated using the FRAs and the results are compared to those using traditional methods. The paper proposes trajectory description techniques by using extremely smooth polynomial functions of time, which can describe point-to-point attitude maneuvers in a realizable and accurate manner with the help of unique FRA features. In addition, new controller design techniques using the FRAs are developed by combining the proposed interpolation techniques with a model predictive control framework. The proposed techniques are validated through their attitude control applications for an aggressive point-to-point maneuver. Conclusively, the FRAs provide much more flexibility than quaternions and Euler angles when describing kinematics, generating trajectories, and designing attitude controllers for spacecraft.
목차
Abstract
1. Introduction
2. Attitude Kinematics with FRAs
3. Interpolation of Angular Orientation
4. Attitude Trajectory Generation Using Finite Rotation Angles
5. Attitude Controller Design Using Finite Rotation Angles
6. Conclusion
References
참고문헌 (23)
참고문헌 신청
Stevens, B. R. and Lewis, F. L., Aircraft Control and Simulation, John Wiley & Son, Inc., New York, 1992, pp. 39-44.
Stengel, R. F., Flight Dynamics, Princeton University Press, Princeton, 2004, pp. 182-187.
Wie, B., Space Vehicle Dynamics and Control, 2nd ed., AIAA Education Series, AIAA, New York, 2008, pp. 329-340, 404-486.
Felippa, C. A. and Haugen, B., “Unified Formulation of Small-Strain Corotational Finite Elements: I. Theory”, Center for Aerospace Structures, Rept. CU-CAS-05-02, College of Engineering, University of Colorado, January 2005.
Verthm, J. M. V. and Bishop, L. M., Essential Mathematics for Games and Interactive Applications: A Programmer’s Guide, 2nd ed., Elsevier Inc., New York, 2008, pp. 141-150, 431-492.
Stengel, R. F., Flight Dynamics, Princeton University Press, Princeton, 2004, pp. 182-187.
Wie, B., Space Vehicle Dynamics and Control, 2nd ed., AIAA Education Series, AIAA, New York, 2008, pp. 329-340, 404-486.
Felippa, C. A. and Haugen, B., “Unified Formulation of Small-Strain Corotational Finite Elements: I. Theory”, Center for Aerospace Structures, Rept. CU-CAS-05-02, College of Engineering, University of Colorado, January 2005.
Verthm, J. M. V. and Bishop, L. M., Essential Mathematics for Games and Interactive Applications: A Programmer’s Guide, 2nd ed., Elsevier Inc., New York, 2008, pp. 141-150, 431-492.
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