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Journal ArticleDOI

Closed-form solutions to constrained control allocation problem

Kenneth A. Bordingnon, +1 more
- 01 Sep 1995 - 
- Vol. 18, Iss: 5, pp 1000-1007
TLDR
This paper describes the results of recent research into the problem of allocating several flight control effectors to generate moments acting on a flight vehicle using various generalized inverse solutions and a hybrid solution utilizing daisy chaining.
Abstract
This paper describes the results of recent research into the problem of allocating several flight control effectors to generate moments acting on a flight vehicle. The results focus on the use of various generalized inverse solutions and a hybrid solution utilizing daisy chaining. In this analysis, the number of controls is greater than the number of moments being controlled, and the ranges of the controls are constrained to certain limits. The control effectors are assumed to be individually linear in their effects throughout their ranges of motion and independent of one another in their effects. A standard of comparison is developed based on the volume of moments or moment coefficients a given method can yield using admissible control deflections. Details of the calculation of the various volumes are presented. Results are presented for a sample problem involving 10 flight control effectors. The effectivenesses of the various allocation schemes are contrasted during an aggressive roll about the velocity vector at low dynamic pressure. The performance of three specially derived generalized inverses, a daisy-chaining solution, and direct control allocation are compared.

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Citations
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BookDOI

Handbook of Marine Craft Hydrodynamics and Motion Control: Fossen/Handbook of Marine Craft Hydrodynamics and Motion Control

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Control allocation—A survey

TL;DR: The objective of the present paper is to survey control allocation algorithms, motivated by the rapidly growing range of applications that have expanded from the aerospace and maritime industries, where control allocation has its roots, to automotive, mechatronics, and other industries.
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Fault tolerant control using sliding modes with on-line control allocation ☆

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.
References
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Journal ArticleDOI

The quickhull algorithm for convex hulls

TL;DR: This article presents a practical convex hull algorithm that combines the two-dimensional Quickhull algorithm with the general-dimension Beneath-Beyond Algorithm, and provides empirical evidence that the algorithm runs faster when the input contains nonextreme points and that it used less memory.
Book

Aircraft Control and Simulation

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

The theory of linear economic models

TL;DR: Gale as discussed by the authors provides a complete and lucid treatment of important topics in mathematical economics which can be analyzed by linear models, including games, linear programming, and the Neumann model of growth.
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The Theory of Linear Economic Models

TL;DR: Gale as mentioned in this paper provides a complete and lucid treatment of important topics in mathematical economics which can be analyzed by linear models, including games, linear programming, and the Neumann model of growth.
Journal ArticleDOI

Nonlinear inversion flight control for a supermaneuverable aircraft

TL;DR: In this article, the authors discuss the use of nonlinear dynamic inversion in the design of a flight control system for a Superman aircraft and compare it with a more conventional, gain-scheduled system and yield better performance in terms of lateral acceleration, sideslip, and control deflections.