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作者:B. R. Andrievsky , N. V. Kuznetsov , G. A. Leonov
来源:[J].Journal of Computer and Systems Sciences International(IF 0.249), 2017, Vol.56 (3), pp.455-470
摘要:This review is devoted to the control problem with constraints on the magnitude and rate of change of the control action in aircraft control systems. In engineering practice, it is accepted to use actuators with a sufficiently large level of magnitude and energy supply. Theo...
作者:Nikolai Botkin , Varvara Turova , Johannes Diepolder ...
来源:[J].Dynamic Games and Applications, 2017, Vol.7 (4), pp.594-608
摘要:This paper addresses the analysis of aircraft control capabilities during the cruise phase (flying at the established level with practically constant configuration and speed) in the presence of windshears. The study uses a point-mass aircraft model describing flight in a vertical...
作者:D. Henry , J. Cieslak , A. Zolghadri ...
来源:[J].Control Engineering Practice(IF 1.669), 2014, Vol.31, pp.183-199
摘要:Abstract(#br)The presented work is undertaken within the FP7-ADDSAFE (Advanced Fault Diagnosis for Sustainable Flight Guidance and Control) project, a European collaborative project that aims to propose new fault diagnosis techniques for AIRBUS aircraft that could significantly...
作者:Rihab El Houda Thabet , Christophe Combastel , Tarek Raïssi ...
来源:[J].International Journal of Control(IF 1.008), 2015, Vol.88 (9), pp.1878-1894
摘要:The paper develops a set membership detection methodology which is applied to the detection of abnormal positions of aircraft control surfaces. Robust and early detection of such abnormal positions is an important issue for early system reconfiguration and overall optimisation of...
作者:Qing Wang , Ligang Gong , Chaoyang Dong ...
来源:[J].Aerospace Science and Technology(IF 0.873), 2019, Vol.93
摘要:Abstract(#br)This paper investigates the control problem of a morphing aircraft with variable sweep wings based on switched nonlinear systems and adaptive dynamic programming (ADP). The longitudinal altitude motion of the morphing aircraft is first modeled as switched nonlinear ...
作者:Zhaohua Yang , Wen Jiang , Xia Liu ...
来源:[J].Journal of the Franklin Institute(IF 2.418), 2016
摘要:Abstract(#br)A new aircraft guidance law utilizing predictive control algorithm is proposed. Compared with extended proportional navigation guidance law, this guidance law is designed specifically for using against a maneuverable target. It can track the target maneuver effective...
作者:Xinhua Wang , Bijan Shirinzadeh
来源:[J].Mechanical Systems and Signal Processing(IF 1.913), 2014, Vol.46 (2), pp.227-252
摘要:... The theoretical results are confirmed by computer simulations and an experiment on a quadrotor aircraft: (i) the estimation of flying velocity and acceleration from the position measurement; (ii) a control law is designed based on the presented nonlinear differentiator to tr...
作者:L. Van Eykeren , Q.P. Chu
来源:[J].Control Engineering Practice(IF 1.669), 2014, Vol.31, pp.200-210
摘要:Abstract(#br)This paper presents a new approach to Fault Detection and Isolation (FDI) for sensors of aircraft. In the most general case, fault detection of these sensors on modern aircraft is performed by a logic that selects one of, or combines, the three redundant measurements...
作者:Clément Roos , Jean-Marc Biannic , Sophie Tarbouriech ...
来源:[J].Aerospace Science and Technology(IF 0.873), 2010, Vol.14 (7), pp.459-471
摘要:Abstract(#br)As an original alternative to dynamic inversion techniques, a non-standard anti-windup control strategy is developed in this paper in order to improve the on-ground control system of a civilian aircraft. Using a linear fractional representation (LFR) of the aircraft ...

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