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논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 발행연도
- 2008.10
- 수록면
- 169 - 174 (6page)
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초록· 키워드
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This paper discussed a nonlinear trajectory tracking problem for stratospheric airship platform and a novel approach of the nonlinear control scheme is applied. Target airship model is the 200m stratospheric airship platform capable of flying upto 20 km altitude. Full 6-DOF nonlinear dynamics of unmanned airship are defined according to the target airship’ configuration including the moving windfield. Based on this airship model, a backstepping design formulation for the trajectory tracking control is described. The tracking control strategy of vectorial backstepping is applied to derive the tracking control law and global asymptotically stability is proved by Lyapunov stability analysis. Finally, numerical simulations have been carried out to assess the performance of the proposed tracking controller.
목차
Abstract
1. INTRODUCTION
2. TARGET AIRSHIP (VIA-200)
3. NONLINEAR DYNAMIC MODEL
4. BACKSTEPPING DESIGN FOR TRAJECTORY TRACKING CONTROL
5. TRAJECTORY TRACKING RESULTS
6. CONCLUSTIONS AND REMARKS
REFERENCES
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UCI(KEPA) : I410-ECN-0101-2014-569-000982573