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2
Published in 2020 at "Nonlinear Dynamics"
DOI: 10.1007/s11071-020-05707-2
Abstract: A new adaptive neural control method, with the actuators multiple constraints of amplitude and rate into consideration, is proposed in this paper for the flexible air-breathing hypersonic vehicle (AHV). In order to better reflect the…
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Keywords:
control;
neural control;
new adaptive;
control law ... See more keywords
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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.02.029
Abstract: Abstract A new type of earth observation mission using a spacecraft with rotational payload is introduced in this paper. The kinematic and dynamic equations for the nadir-aligned attitude tracking problem are derived in the presence…
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Keywords:
misaligned rotational;
control;
control spacecraft;
control law ... See more keywords
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1
Published in 2019 at "Chinese Journal of Aeronautics"
DOI: 10.1016/j.cja.2019.07.001
Abstract: Abstract A CFD-based Numerical Virtual Flight (NVF) simulator is presented, which integrates an unsteady flow solver on moving hybrid grids, a Rigid-Body Dynamics (RBD) solver and a module of the Flight Control System (FCS). A…
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Keywords:
control;
flight;
simulator;
control law ... See more keywords
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1
Published in 2017 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2017.08.1645
Abstract: Abstract In this paper the modeling and control law design for a quadcopter tiltorotor UAV are considered. The problem is developed in a geometric setting to obtain an intrinsic control law which achieves local exponential…
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Keywords:
quadcopter;
control;
geometric tracking;
tracking control ... See more keywords
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Published in 2018 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2018.07.310
Abstract: Abstract In the present paper, a mathematical model for a portfolio is proposed. This model is valid for operations of buying and selling shares of an asset in constant periods of time, additionally, it has…
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Keywords:
portfolio modeling;
portfolio;
control;
control theory ... See more keywords
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1
Published in 2018 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2018.12.083
Abstract: Abstract Model predictive control (MPC) of a separated flow around a circular cylinder at a low Reynolds number is presented in this paper. In order to reduce online computational cost, we propose to extract an…
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Keywords:
model predictive;
control;
cylinder;
predictive control ... See more keywords
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1
Published in 2019 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2019.12.049
Abstract: Abstract In this paper we present an approach for testing flight control laws with optimal disturbances using differential game theory. The approach is based on a state constrained differential game formulation in which the criterion…
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Keywords:
control law;
control;
flight control;
game ... See more keywords
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1
Published in 2020 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2020.12.1927
Abstract: Abstract This article presents the design and evaluation of a robust C⁎ control law through Hardware-In-the-Loop Simulation (HILS) of JAXA’s research aircraft called Multi-Purpose Aviation Laboratory (MuPAL-α). The C⁎ control law, which is a widely…
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Keywords:
evaluation robust;
robust control;
control;
control law ... See more keywords
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Published in 2020 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2020.12.1946
Abstract: Abstract The problem of magnetic detumbling, also known as magnetic momentum unloading, is considered. The objective is to stabilize a rigid spacecraft angular velocity to zero only through magnetic actuation, i.e. magneto-torquers. We propose a…
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Keywords:
law;
rigid spacecraft;
generalized control;
control law ... See more keywords
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Published in 2019 at "IEEE Control Systems Letters"
DOI: 10.1109/lcsys.2019.2919309
Abstract: Recently, a predictor feedback control strategy has been reported for the feedback stabilization of a class of infinite-dimensional Riesz-spectral boundary control systems exhibiting a finite number of unstable modes by means of a delay boundary…
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Keywords:
boundary control;
control;
feedback stabilization;
control law ... See more keywords
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3
Published in 2022 at "IEEE Control Systems Letters"
DOI: 10.1109/lcsys.2021.3137714
Abstract: This letter considers a robust sliding mode control method for a spacecraft attitude control. The design of the control law is based on the reaching law approach for continuous-time systems. A novel method is proposed…
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Keywords:
reaching law;
control law;
law;
based smc ... See more keywords