Fuzzy logic PID controller for missile terminal guidance

Gonsalves, Paul; Çağlayan, Alper

doi:10.1109/isic.1995.525086

Cited by 13 publications

(6 citation statements)

References 10 publications

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“…Proportional-integral-derivative (PID) controller and its variants have been well established not only as shown in textbooks [1,2] and research papers [3,4] but also witnessed by their dominant roles in industrial applications, especially in missile guidance and control problems [5,6]. Rogers [5] stated that the classical PID controller is effective to amplify the commanded acceleration before feeding it to the high-order missile control system.…”

Section: Introductionmentioning

confidence: 99%

Application of PID controller to 2D differential geometric guidance problem

Jing

2007

J. Control Theory Appl.

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This paper presents the application of the proportional-integral-derivative (PID) controller to the flight control system (FCS) for two-dimensional (2D) differential geometric (DG) guidance and control problem. In particular, the performance of the designed FCS is investigated. To this end, the commanded angle-of-attack is firstly developed in the time domain using the classical DG formulations. Then, the classical PID controller is introduced to develop a FCS so as to form the 2D DG guidance and control system, and the PID controller parameters are determined by the Ziegler-Nichols method as well as the Routh-Hurwitz stability algorithm to guarantee the convergence of the system error. The results demonstrate that the designed controller yields a fast responding system, and the resulting DG guidance and control system is viable and effective in a realistic missile defense engagement.

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Section: Introductionmentioning

confidence: 99%

Application of PID controller to 2D differential geometric guidance problem

Jing

2007

J. Control Theory Appl.

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show abstract

Section: Introductionmentioning

confidence: 99%

Application of PID Controller to 2D Differential Geometric Guidance and Control Problem

Jing

2006

2006 Chinese Control Conference

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This paper presents the application of the proportional-integral-derivative (PID) controller to the development of the flight control system (FCS) for two-dimensional (2D) differential geometric (DG) guidance and control problem. In particular, the performance of the designed FCS is investigated. To this end, the commanded angle-of-attack (AOA) is firstly developed in the time domain using the classical DG formulations. Then, the classical PID controller is introduced to develop a FCS so as to form the 2D DG guidance and control system, and the PID controller parameters are determined by the Ziegler-Nichols method as well as the Routh-Hurwitz stability algorithm to guarantee a fast convergence of the system error. The results demonstrate that the designed controller yields a fast responding FCS, and the resulting DG guidance and control system is viable and effective in a realistic missile defense engagement.

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“…Recently, FLC has been applied to guidance systems [7][8][9]. However, these fuzzy-logic-based guidance law design methods are based on fuzzy inference rules that are constructed based on the qualitative aspects of human knowledge.…”

Section: Introductionmentioning

confidence: 99%

Self-organizing fuzzy learning CLOS guidance law design

Lin

Hsu²,

Mon³

2003

IEEE Trans. Aerosp. Electron. Syst.

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A new self-organizing fuzzy logic control (SOFLC) design method is proposed. The proposed method is applied to the command line-of-sight (CLOS) guidance law design. The SOFLC contains two sets of fuzzy inference logic. One is the fuzzy logic controller and the other is the rule modifier. The new learning method of the rule modifier is developed based on a fuzzy learning algorithm. The modification value of each rule is based on the fuzzy firing weight, so that learning of the rule bases is reasonable. Finally, two engagement scenarios are examined, and a comparison between a fuzzy logic control (FLC), an optimal learning FLC, and the proposed SOFLC CLOS guidance laws is made. Simulation results show that the proposed SOFLC guidance law can achieve better guidance performance than the other guidance laws.

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Fuzzy logic PID controller for missile terminal guidance

Cited by 13 publications

References 10 publications

Application of PID controller to 2D differential geometric guidance problem

Application of PID controller to 2D differential geometric guidance problem

Application of PID Controller to 2D Differential Geometric Guidance and Control Problem

Self-organizing fuzzy learning CLOS guidance law design

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