Technical Papers
Nov 30, 2023

Three-Dimensional Composite Approach Angle Constrained Guidance Law with Actuator Lag Consideration

Publication: Journal of Aerospace Engineering
Volume 37, Issue 2

Abstract

This paper considers the problem of unmanned aerial vehicle (UAV) aerial collision net recovery in a three-dimensional non-decoupling environment and approach angle constraint. A robust control-observer framework-based guidance law was designed via the nonsingular fast terminal sliding mode control (NFTSMC) technique and adaptive sliding mode disturbance observer (ASMDO). To estimate the disturbance of the guidance system in finite time, an ASMDO is presented in which the parameters are autonomously adjustable according to the estimation error. The proposed control implementation uses the nonsingular fast terminal sliding mode (NFTSM) technique to drive the line-of-sight (LOS) angle error and LOS angular rate fast convergence under model coupling and external disturbance. Furthermore, regarding the actuator of UAV with second-order dynamic, a backstepping guidance law to compensate for actuator dynamics is proposed with the aid of a finite-time converged differentiator, which can estimate directly the derivative of the virtual control law and guarantee the finite-time convergent characteristic of the partially integrated guidance and control system. Simulation studies and comparisons verified the efficiency of the proposed guidance law in the presence of a complex disturbance lump.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

This work was supported by the Natural Science Foundation of China (Grant No. 52272358).

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 2March 2024

History

Received: Dec 14, 2022
Accepted: Sep 18, 2023
Published online: Nov 30, 2023
Published in print: Mar 1, 2024
Discussion open until: Apr 30, 2024

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Yuchen Wang
Ph.D. Candidate, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.
Qinghan Zeng
Professor, Scientific and Technical Center for Innovation, Unit 32178 of the PLA, Beijing 100012, China.
Zhengjia Xu
Postdoctoral Researcher, School of Aerospace, Transport and Manufacturing, Cranfield Univ., Cranfield MK430AL, UK.
Beibei Li
Assistant Engineer, Unit 32381 of the PLA, Beijing 100072, China.
Associate Professor, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China (corresponding author). ORCID: https://orcid.org/0000-0002-6941-2236. Email: [email protected]

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