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Formation Flying with Nonlinear Partial Integrated Guidance and Control

Padhi, Radhakant and Rakesh, PR and Venkataraman, R (2015) Formation Flying with Nonlinear Partial Integrated Guidance and Control. In: IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 50 (4). pp. 2847-2859.

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Official URL: http://dx.doi.org/ 10.1109/TAES.2014.120719

Abstract

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.

Item Type: Journal Article
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Additional Information: Copy right for this article belongs to the IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC, 445 HOES LANE, PISCATAWAY, NJ 08855-4141 USA
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 28 Jan 2015 04:37
Last Modified: 28 Jan 2015 04:37
URI: http://eprints.iisc.ernet.in/id/eprint/50755

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