Maneuver Control Strategies to Maximize Prediction Errors in Ballistic Middle Phase

Guo, Yang; Yao, Yu; Wang, Shicheng; Yang, Baoqing; He, Fenghua; Zhang, Peng

doi:10.2514/1.56818

Cited by 24 publications

(8 citation statements)

References 21 publications

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“…Many guidance applications of control theory are presented in early studies [40–42]. As the terminal interception process of the aircraft is a typical finite‐time process, the control commands and manoeuvres of the aircraft must be completed within the finite‐time interval, else these instructions will be invalid.…”

Section: Examplesmentioning

confidence: 99%

Finite‐time bounded stabilisation for linear systems with finite‐time H ₂ ‐gain constraint

Zhang

Guo

Wang

et al. 2020

IET Control Theory & Applications

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Section: Examplesmentioning

confidence: 99%

Finite‐time bounded stabilisation for linear systems with finite‐time H ₂ ‐gain constraint

Zhang

Guo

Wang

et al. 2020

IET Control Theory & Applications

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“…In view of the above analysis, this study extends the finite-time theory to a SLS, and conduct the stability analysis of both states and output concurrently, which is the conspicuous improvement compared with the results derived in the current study. As a matter of fact, solving the problem of the SLS satisfying both the FTB and FTOS can allow practical engineering applications to be better achieved [32]- [34].…”

Section: Introductionmentioning

confidence: 99%

Finite–Time Output Stability of Impulse Switching System With Norm–Bounded State Constraint

et al. 2019

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This paper discusses the finite-time output stability (FTOS) for the impulse switching linear system (SLS) when the norm-bounded state constraint is simultaneously considered during a scheduled finite-time period. This system is a typical hybrid system whose state trajectory instantaneously jumps according to a predetermined resetting law. The sufficient conditions of both state boundedness and output stability are proposed for the SLS in finite-time period when two typical classes of input signals are involved. Based on the linear matrix inequality, the design method of a controller using state feedback is represented to ensure state boundedness and output stability concurrently for the closed-loop system, which can effectively avoid states and the output reaching large and unacceptable values at certain points in finite time. An effective solution to the controller using a linear discretization approach is also achieved. The two simulation examples verify the proposed methods.

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“…For a physical process finished in a finite-time interval, finite-time control theory may be more effective, since it only focuses on the concerned time interval and the performance indices are always defined in the concerned finite-time interval [23]. Furthermore, there have been some researches applying finite-time control theory for the terminal guidance problems in recent years [24][25][26][27][28][29][30]. Hence, the finite-time control methods will be used to solve the triangle interception problems, as dealt with in this paper.…”

Section: Introductionmentioning

confidence: 99%

Triangle Interception Scenario: A Finite-Time Guidance Approach

Guo

et al. 2016

International Journal of Aerospace Engineering

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Considering an aircraft threatened by an interceptor, one of the effective penetration strategies is to release a Defender from the aircraft to confront the interceptor. In this case, the aircraft, the Defender, and the interceptor constitute the three-body guidance relationship, and the cooperation of the aircraft and its Defender to achieve the best tactical effects turns into a concerned problem. This paper studies the triangle interception guidance problem via the finite-time theory. The paper presents linear system Input-Output Finite-Time Stabilization (IO-FTS) method. The sufficient conditions of the linear system, being IO-FTS, under Finite-Time Boundedness (FTB) constraint are proposed, by which the state feedback controllers design method is obtained, via Linear Matrix Inequalities (LMIs). The triangle interception guidance problems are studied in three different cases, where the proposed methods are applied to the guidance design. The simulation results illustrate the effectiveness of the proposed methods.

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Maneuver Control Strategies to Maximize Prediction Errors in Ballistic Middle Phase

Cited by 24 publications

References 21 publications

Finite‐time bounded stabilisation for linear systems with finite‐time H ₂ ‐gain constraint

Finite‐time bounded stabilisation for linear systems with finite‐time H ₂ ‐gain constraint

Finite–Time Output Stability of Impulse Switching System With Norm–Bounded State Constraint

Triangle Interception Scenario: A Finite-Time Guidance Approach

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Maneuver Control Strategies to Maximize Prediction Errors in Ballistic Middle Phase

Cited by 24 publications

References 21 publications

Finite‐time bounded stabilisation for linear systems with finite‐time H 2 ‐gain constraint

Finite‐time bounded stabilisation for linear systems with finite‐time H 2 ‐gain constraint

Finite–Time Output Stability of Impulse Switching System With Norm–Bounded State Constraint

Triangle Interception Scenario: A Finite-Time Guidance Approach

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Product

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Finite‐time bounded stabilisation for linear systems with finite‐time H ₂ ‐gain constraint

Finite‐time bounded stabilisation for linear systems with finite‐time H ₂ ‐gain constraint