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Docking control for probe-drogue refueling: An additive-state-decomposition-based output feedback iterative learning control method

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posted on 2019-11-20, 09:57 authored by Jinrui Ren, Quan Quan, Cunjia LiuCunjia Liu, Kai-Yuan Cai
Designing a controller for the docking maneuver in Probe-Drogue Refueling (PDR) is an important but challenging task, due to the complex system model and the high precision requirement. In order to overcome the disadvantage of only feedback control, a feedforward control scheme known as Iterative Learning Control (ILC) is adopted in this paper. First, Additive State Decomposition (ASD) is used to address the tight coupling of input saturation, nonlinearity and the property of NonMinimum Phase (NMP) by separating these features into two subsystems (a primary system and a secondary system). After system decomposition, an adjoint-type ILC is applied to the Linear Time-Invariant (LTI) primary system with NMP to achieve entire output trajectory tracking, whereas state feedback is used to stabilize the secondary system with input saturation. The two controllers designed for the two subsystems can be combined to achieve the original control goal of the PDR system. Furthermore, to compensate for the receiver-independent uncertainties, a correction action is proposed by using the terminal docking error, which can lead to a smaller docking error at the docking moment. Simulation tests have been carried out to demonstrate the performance of the proposed control method, which has some advantages over the traditional derivative-type ILC and adjoint-type ILC in the docking control of PDR.

Funding

National Natural Science Foundation of China ( No.: 61473012)

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Published in

Chinese Journal of Aeronautics

Volume

33

Issue

3

Pages

1016 - 1025

Publisher

Elsevier BV

Version

  • VoR (Version of Record)

Rights holder

© Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics

Publisher statement

This is an Open Access Article. It is published by Elsevier under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/

Acceptance date

2019-11-08

Publication date

2019-11-16

Copyright date

2019

ISSN

1000-9361

Language

  • en

Depositor

Dr Cunjia Liu. Deposit date: 17 November 2019

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