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Formation flying with nonlinear partial integrated guidance and control (2014)

Institute of Electrical and Electronics Engineers (IEEE)

In: IEEE Transactions on Aerospace and Electronic Systems

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Publication Date: 2014-12-13

Description: 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.

Print ISSN: 0018-9251

Electronic ISSN: 1557-9603

Topics: Electrical Engineering, Measurement and Control Technology , Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics

Published by Institute of Electrical and Electronics Engineers (IEEE)

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