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.
Formation flying with nonlinear partial integrated guidance and control
IEEE Transactions on Aerospace and Electronic Systems ; 50 , 4 ; 2847-2859
01.10.2014
3246062 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Formation Flying of UAVs with Dynamic Inversion Based Partial Integrated Guidance and Control
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