利用无模型自适应控制为三级卫星运载器设计新颖的综合制导和控制装置

IF 1 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Mohammadreza Yaseri, Alireza Basohbat Novinzadeh
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引用次数: 0

摘要

本文提出了一种无模型自适应控制方法,用于原型三级卫星运载火箭的次优制导修正和控制。为此,我们考虑了系统模型的额定制导,并为单输入多输出系统设计了自适应控制,该系统在输入和输出率方面受到风干扰和测量噪声的影响。然后,在进行制导修正后,估算出系统的微分模型,并在一些有利可图的性能约束条件下实现控制策略,使卫星进入理想的圆形轨道。仿真结果很容易揭示所提方法的效率及其对系统不确定性的鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Novel integrated guidance and control design for a three-stage satellite carrier using model-free adaptive control
A model-free adaptive control is proposed for suboptimal guidance correction and control of a prototypical three-stage satellite carrier. For this sake, we consider a nominal guidance for the model of the system and design the adaptive control for a single-input multi-output system exposed to wind disturbance and measurement noise in the rates of inputs and outputs. Then, subsequent to the guidance correction, a differentiation model of the system is estimated and the control policy is realized under some profitable performance constraints to set the satellite in a desirable circular orbit. The simulation results readily reveal the efficiency of the proposed method and its robustness to uncertainties in the system.
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来源期刊
CiteScore
2.40
自引率
18.20%
发文量
212
审稿时长
5.7 months
期刊介绍: The Journal of Aerospace Engineering is dedicated to the publication of high quality research in all branches of applied sciences and technology dealing with aircraft and spacecraft, and their support systems. "Our authorship is truly international and all efforts are made to ensure that each paper is presented in the best possible way and reaches a wide audience. "The Editorial Board is composed of recognized experts representing the technical communities of fifteen countries. The Board Members work in close cooperation with the editors, reviewers, and authors to achieve a consistent standard of well written and presented papers."Professor Rodrigo Martinez-Val, Universidad Politécnica de Madrid, Spain This journal is a member of the Committee on Publication Ethics (COPE).
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