Open Access
Issue
JNWPU
Volume 39, Number 5, October 2021
Page(s) 995 - 1004
DOI https://doi.org/10.1051/jnwpu/20213950995
Published online 14 December 2021
  1. Richard Colgren, Dale Enns. Dynamic inversion applied to the F-117A[C]//Modeling and Simulation Technologies Conference, 1997 [Google Scholar]
  2. Menon P P, Lowenberg M H, Herrmann G, et al. Experimental implementation of a nonlinear dynamic inversion controller with antiwindup[J]. Journal of Guidance Control and Dynamics, 2013, 36(4): 1035–1046 [Article] [Google Scholar]
  3. Lombaerts Thomas, Kaneshige John, Schuet Stefan, et al. Dynamic inversion based full envelope flight control for an evtol vehicle using a unified framewor[C]//AIAA Scitech 2020 Forum [Google Scholar]
  4. Lungu M. Auto-landing of UAVs with variable centre of mass using the backstepping and dynamic inversion control[J]. Aerospace Science and Technology, 2020, 103: 105912 [Article] [Google Scholar]
  5. Simplicio P, Pavel M D, Van Kampen E, et al. An acceleration measurements-based approach for helicopter nonlinear flight control using incremental nonlinear dynamic inversion[J]. Control Engineering Practice, 2013, 21(8): 1065–1077 [Article] [Google Scholar]
  6. Lu Peng, Van Kampen Erikjan, De Visser Cornelis, et al. Aircraft fault-tolerant trajectory control using incremental nonlinear dynamic inversion[J]. Control Engineering Practice, 2016, 57: 126–141 [Article] [Google Scholar]
  7. Sieberling S, Chu Q P, Mulder J A, et al. Robust flight control using incremental nonlinear dynamic inversion and angular acceleration prediction[J]. Journal of Guidance Control and Dynamics, 2010, 33(6): 1732–1742 [Article] [Google Scholar]
  8. Tetsujiro Ninomiya, Yoshikazu Miyazawa. Neural network based adaptive control with hierarchy structured dynamic inversion applied to nonlinear aircraft model[C]//AIAA Guidance, Navigation, and Control Conference, 2010 [Google Scholar]
  9. Lakshmikanth G S, Padhi R, Watkins J M, et al. Adaptive flight-control design using neural-network-aided optimal nonlinear dynamic inversion[J]. Journal of Aerospace Information Systems, 2014, 11(11): 785–806 [Article] [Google Scholar]
  10. Cao C, Hovakimyan N. Design and analysis of a novel L1 adaptive controller, part I: control signal and asymptotic stability[C]//American Control Conference, 2006 [Google Scholar]
  11. Li Z, Hovakimyan N. L1 adaptive controller for MIMO systems with unmatched uncertainties using modified piecewise constant adaptation law[C]//IEEE Conference on Decision & Control, 2012: 7303–7308 [Google Scholar]
  12. Zhou Yan, Liu Huiying, Li Jing. L1 adaptive for aircraft lateral fault tolerant control with actuator failure[J]. Journal of Northwestern Polytechnical University, 2019, 37(5): 937–942 [Article] (in Chinese) [Google Scholar]
  13. Gao Li, Wu Wenhai, Mei Dan, et al. Design of L1 adaptive controller for lateral-directional automatic carrier landing[J]. Flight Dynamics, 2016(4): 41–45 [Article] (in Chinese) [Google Scholar]
  14. Li Yu, Liu Xiaoxiong, Li Jikuan, et al. Design the characteristic analysis of L1 adaptive longitudinal control for carrier-based landing[J]. Computer Measurement & Control, 2018, 26(12): 120–124 [Article] (in Chinese) [Google Scholar]
  15. Pomet J B, Praly L. Adaptive nonlinear regulation: estimation from the Lyapunov equation[J]. IEEE Trans on Automatic Control, 1992, 37(6): 729–740 [Article] [Google Scholar]
  16. Nguyen L T, Ogburn M E, Gilbert W P, et al. Simulator study of a stall/post-stall characteristics of a fighter airplane with relaxed longitudinal static stability[R]. TP1538, NASA, Hampton, VA, 1979 [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.