Open AccessDissertation
Application of Control Allocation Methods to Linear Systems with Four or More Objectives
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The article was published on 2002-06-11 and is currently open access. It has received 37 citations till now. The article focuses on the topics: Linear system & Linear programming.read more
Citations
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Journal ArticleDOI
Fault tolerant control using sliding modes with on-line control allocation ☆
Halim Alwi,Christopher Edwards +1 more
TL;DR: In this paper, an on-line sliding mode control allocation scheme for fault tolerant control is proposed, where the effectiveness level of the actuators is used to redistribute the control signals to the remaining actuators when a fault or failure occurs.
Backstepping and control allocation with applications to flight control
TL;DR: In this paper, an adaptive backstepping and nonlinear observer design method is proposed for nonlinear control problems in flight control and the results are presented in a general framework and can also be applied to other areas.
Journal ArticleDOI
Spacecraft thruster control allocation problems
P.A. Servidia,R.S. Pena +1 more
TL;DR: A control allocation algorithm based on a subgradient optimization, which is shown to be faster than existing allocators, is proposed and proposed.
Fault-tolerant Control Allocation for Multirotor Helicopters Using Parametric Programming
TL;DR: In this article, the authors proposed a control allocator for fault-tolerant flight of multi-rotor helicopter with the following points: given the configuration of the multirotor vehicle, the maximum torque that can be produced on each vehicle axis, and a method to investigate the static controllability of the vehicle in any arbitrary fault configuration is described.
Journal ArticleDOI
Aircraft Load Alleviation During Maneuvers Using Optimal Control Surface Combinations
TL;DR: In this paper, an optimal strategy of the control surface use, which leaves the initial flight behavior unmodified but alleviates a structural load during a selected maneuver, was proposed to alleviate the bending moment at the external wing during a sudden and strong roll maneuver.
References
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Book
Linear and nonlinear programming
David G. Luenberger,Yinyu Ye +1 more
TL;DR: Strodiot and Zentralblatt as discussed by the authors introduced the concept of unconstrained optimization, which is a generalization of linear programming, and showed that it is possible to obtain convergence properties for both standard and accelerated steepest descent methods.
Book
Aircraft Control and Simulation
Brian L. Stevens,Frank L. Lewis +1 more
TL;DR: Equations of Motion Building the Aircraft Model Basic Analytical and Computational Tools Aircraft Dynamics and Classical Design Techniques Modern Design Techniques Robustness and Multivariable Frequency-Domain Techniques Digital Control Appendices Index.
Book
Primal-Dual Interior-Point Methods
TL;DR: This chapter discusses Primal Method Primal-Dual Methods, Path-Following Algorithm, and Infeasible-Interior-Point Algorithms, and their applications to Linear Programming and Interior-Point Methods.
Book
Nonlinear Systems: Analysis, Stability, and Control
TL;DR: In this article, the authors compare Linear vs. Nonlinear Control of Differential Geometry with Linearization by State Feedback (LSF) by using Linearization and Geometric Non-linear Control (GNC).