Formation Flying with Nonlinear Partial Integrated Guidance and Control

被引：13

作者：

Padhi, Radhakant ^{[1
]}

Rakesh, P. R. ^{[1
]}

Venkataraman, R. ^{[1
]}

机构：

[1] Indian Inst Sci, Dept Aerosp Engn, Bangalore 560012, Karnataka, India

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2014年 / 50卷 / 04期

关键词：

SLIDING-MODE CONTROL;

D O I：

10.1109/TAES.2014.120719

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Using the dynamic inversion philosophy, a nonlinear partial integrated guidance and control approach is presented in this paper for formation flying. It is based on the evolving philosophy of integrated guidance and control. However, it also retains the advantages of the conventional guidance then control philosophy by retaining the timescale separation between translational and rotational dynamics explicitly. Simulation studies demonstrate that the proposed technique is effective in bringing the vehicles into formation quickly and maintaining the formation.

引用

页码：2847 / 2859

页数：13

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