Aircraft Turn Maneuver using Bifurcation Analysis and Nonlinear Dynamic Inversion Control Technique

Khatri, AK (2011) Aircraft Turn Maneuver using Bifurcation Analysis and Nonlinear Dynamic Inversion Control Technique. In: NATIONAL CONFERENCE ON ADVANCED CONTROL IN ENGINEERING SYSTEMS , 21-23 September 2011, M.S.Ramaiah Institute of Technology, Bangalore.

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Abstract

This paper demonstrates the application of bifurcation analysis and continuation technique based methodology and nonlinear dynamic inversion (NDI) control technique for designing aircraft maneuvers. A turning maneuver to the minimum sustained turn radius flight condition for F- 18/ HARV aircraft model has been chosen to exemplify the proposed approach. A constrained bifurcation analysis based procedure is first carried out to construct the turn maneuver. The information available from bifurcation analysis is then used to specify the reference inputs for the NDI controller to switch the aircraft between the desired trim points. Closed-loop simulation results are also presented to show the effectiveness of the proposed methodology for designing aircraft maneuvers.

Item Type: Conference or Workshop Item (Paper)
Subjects: AERONAUTICS > Aircraft Stability and Control
Depositing User: Amit Amit Khatri
Date Deposited: 06 Mar 2014 06:33
Last Modified: 06 Mar 2014 06:33
URI: http://nal-ir.nal.res.in/id/eprint/11933

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