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Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation

Published online by Cambridge University Press:  07 August 2019

X. L. Ai Open the ORCID record for X. L. Ai [Opens in a new window] ,
Y. C. Shen  and
L. L. Wang
X. L. Ai*
Affiliation:
School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081, China
Y. C. Shen
Affiliation:
Beijing Institute of Electronic System Engineering, Beijing, 100854, China
L. L. Wang
Affiliation:
Beijing Institute of Space Long March Vehicle, Beijing, 100076, China
*
[email protected]
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Abstract

This paper considers the integrated guidance and control (IGC) problem for impact angle constrained interception against manoeuvring targets with actuator saturation constraint. Based on the backstepping technique, an adaptive IGC law is presented to address this problem, where a fixed-time differentiator is proposed to estimate the derivatives of virtual control inputs to avoid the inherent problem of “explosion of complexity” suffered by the typical backstepping. Furthermore, an auxiliary first-order filter is introduced into the IGC law to cope with the actuator saturation constraint. The stability of the closed-loop system is strictly proved. Finally, the superiority of the proposed IGC law is verified by comparison simulations.

Keywords

Integrated guidance and controlImpact angle constraintActuator saturationAerodynamic uncertaintiesManoeuvring targets
Type
Research Article
Information
The Aeronautical Journal , Volume 123 , Issue 1267 , September 2019 , pp. 1437 - 1453
Copyright
© Royal Aeronautical Society 2019 

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