State-feedback control for full-state constrained nonlinear systems in a prescribed time

Min, Huifang; Shi, Shang

doi:10.1016/j.jfranklin.2024.107052

Journal of the Franklin Institute

2024

DOI: 10.1016/j.jfranklin.2024.107052

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State-feedback control for full-state constrained nonlinear systems in a prescribed time

Huifang Min,

Shang Shi

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2024

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Cited by 1 publication

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Time‐Varying Sliding Mode Based Fixed‐Time Missile Guidance and Attitude Control With Impact Angle Constraints

Wei,

Song

2024

Intl J Robust & Nonlinear

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Considering an unpowered missile diving to intercept a maneuvering target, a novel fixed‐time guidance and attitude control algorithm is proposed. First, the second‐order derivatives of the aerodynamic angles are directly linked to the fin deflections, which can avoid the tracking of missile body angle rate instruction in the traditional methods. Second, a novel fixed‐time time‐varying parameter nonsingular terminal sliding mode guidance law is proposed, which can avoid control input singularity without switching to the polynomial form when the error approaches the origin. Third, a new global time‐varying sliding mode with a predefined convergence time and analytical solution is developed to design the attitude controller. The system states are proved to be fixed‐time convergence based on the Lyapunov stability theory. Six‐degree‐of‐freedom simulations are conducted to validate the superiority of the proposed algorithm in terms of miss distance, impact angle error, interception time and control energy.

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Time‐Varying Sliding Mode Based Fixed‐Time Missile Guidance and Attitude Control With Impact Angle Constraints

Wei,

Song

2024

Intl J Robust & Nonlinear

View full text Add to dashboard Cite

show abstract

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State-feedback control for full-state constrained nonlinear systems in a prescribed time

Cited by 1 publication

References 34 publications

Time‐Varying Sliding Mode Based Fixed‐Time Missile Guidance and Attitude Control With Impact Angle Constraints

Time‐Varying Sliding Mode Based Fixed‐Time Missile Guidance and Attitude Control With Impact Angle Constraints

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