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Contents

Flight control design using incremental nonlinear dynamic inversion with fixed-lag smoothing estimation / Tito J. Ludeña Cervantes ; Seong H. Choi ; Byoung S. Kim 1

Abstract 1

Abbreviation 1

Subscripts 1

1. Introduction 1

2. Incremental Nonlinear Dynamic Inversion 2

3. Smoothing Algorithm 3

3.1. Discrete Kalman Filter 3

3.2. Fixed-lag Smoothing Algorithm 3

4. Flight Control Design using INDI and Smoothing Algorithm 5

4.1. A Control Augmentation System with INDI 5

4.2. Discrete-time Smoother 7

5. Simulation and Results 8

6. Conclusion 12

References 12

권호기사

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Numerical research on the unsteady evolution characteristics of blade tip vortex for helicopter rotor in forward flight Zhou Ye, Fengjiang Zhan, Guohua Xu p. 865-878

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Flight control design using incremental nonlinear dynamic inversion with fixed-lag smoothing estimation Tito J. Ludeña Cervantes, Seong H. Choi, Byoung S. Kim p. 1047-1058

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참고문헌 (17건) : 자료제공( 네이버학술정보 )

참고문헌 목록에 대한 테이블로 번호, 참고문헌, 국회도서관 소장유무로 구성되어 있습니다.
번호 참고문헌 국회도서관 소장유무
1 Bugajski DJ, Enns DF (1992) Nonlinear Control Law with Application to High Angle-of-Attack flight. J Guidance Control Dyn 15(3):761–767. https://doi.org/10.2514/3.20902 미소장
2 Snell SA, Enns DF, Garrard WL (1992) Nonlinear Inversion Flight Control for a SupermaneuverableAircraft. JGuidanceControlDyn 5(4):978–948. https://doi.org/10.2514/3.20932 미소장
3 Kim BS, Calise AJ (1997) Nonlinear Flight control using neural networks. J Guidance Control Dyn 20(1):26–33. https://doi.org/10.2514/2.4029 미소장
4 Navigation and Geodetic System(Switchover to WGS-Based Nautical Charts) 네이버 미소장
5 Sieberling S, Chu QP, Mulder JA (2010) Robust Flight Control using Incremental Nonlinear Dynamic Inversion. J Guidance Control Dyn 33(6):1732–1742. https://doi.org/10.2514/1.49978 미소장
6 Simplício PVM (2011) Helicopter nonlinear flight control: An acceleration measurements-based approach using incremental nonlinear dynamic inversion, Master thesis, Delf University of Technology, SouthHolland, Netherlands. http://resolver.tudelft.nl/uuid:d2ffe4d1-219e-4965-a6b4-debb900ded4c 미소장
7 Slinger BJMM (2016) Attitude control of a small helicopter UAV using incremental nonlinear dynamic inversion, Master thesis, Delf University of Technology, South Holland, Netherlands. http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4 미소장
8 Smeur E, Chu Q, de Croon G (2016) Adaptive incremental nonlinear dynamic inversion for attitude control of micro aerial vehicles. J Guidance Control Dyn. doi 10(2514/1):G001490 미소장
9 Ovaska SJ, Valiviita S (1998) Angular acceleration measurement:a review. IEEE Trans Instrum Meas 47(5):1211–1217. https://doi. org/10.1109/19.746585 미소장
10 Pasanen J, Vainio O, Ovaska SJ (1994) Predictive synchronization and restoration of corrupted velocity samples. Measurement 13:315–324. https://doi.org/10.1016/0263-2241(94)90056-6 미소장
11 Bélanger PR(1992) Estimation of angular velocity and acceleration from shaft encoder measurements. In: Proceedings of the 1992IEEE International Conference on Robotics and Automation, Nice, France, Vol. 1, pp. 585–592. doi: https://doi.org/10.1109/ROBOT. 1992.220228 미소장
12 LevantA(1998) Robust exact differentiation via sliding mode technique. Automatica 34(3):379–384. https://doi.org/10.1016/S0005-1098(97)00209-4 미소장
13 Mendel JM(1986) Lessons in Digital Estimation Theory. Prentice-Hall, Englewood Cliffs, New Jersey,s 1986, Chaps 16–21. 미소장
14 Anderson BDO, Moore JB (1979) Optimal filtering. Prentice-Hall, Englewood Cliffs 미소장
15 Moore JB (1973) Discrete-time fixed-lag smoothing algorithms. Automatica 9(2):163–173. https://doi.org/10.1016/0005-1098(73)90071-X 미소장
16 Iliff KW, Wang KC (1999) Flight-determined subsonic lateraldirectional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives. NASA/TP-1999-206573, NASA Dryden Flight Research Center, Edwards, CA, United States. https://ntrs.nasa.gov/search.jsp?R=19990019364 미소장
17 Bar-Shalom Y, Li RX, Kirubarajan T (2001) Estimation with Applications to Tracking and Navigation, Chap 10. Wiley, New York, p 500 미소장

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