A Fuzzy Technique for Performing Lateral-Axis Formation Flight Navigation Using Wingtip Vortices

Hanson, Curtis E. (2003) A Fuzzy Technique for Performing Lateral-Axis Formation Flight Navigation Using Wingtip Vortices. Technical Report NASA/TM-2003-212033, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

Close formation flight involving aerodynamic coupling through wingtip vortices shows significant promise to improve the efficiency of cooperative aircraft operations. Impediments to the application of this technology include intership communication required to establish precise relative positioning. This report proposes a method for estimating the lateral relative position between two aircraft in close formation flight through real-time estimates of the aerodynamic effects imparted by the leading airplane on the trailing airplane. A fuzzy algorithm is developed to map combinations of vortex-induced drag and roll effects to relative lateral spacing. The algorithm is refined using self-tuning techniques to provide lateral relative position estimates accurate to 14 in., well within the requirement to maintain significant levels of drag reduction. The fuzzy navigation algorithm is integrated with a leader-follower formation flight autopilot in a two-ship F/A-18 simulation with no intership communication modeled. It is shown that in the absence of measurements from the leading airplane the algorithm provides sufficient estimation of lateral formation spacing for the autopilot to maintain stable formation flight within the vortex. Formation autopilot trim commands are used to estimate vortex effects for the algorithm. The fuzzy algorithm is shown to operate satisfactorily with anticipated levels of input uncertainties.

EPrint Type:	NASA Technical Memorandum
Keywords:	Automatic pilot, Drag reduction, Formation flying, Fuzzy system, Wingtip vortex, F-18 AFF, Formation flight
Subjects:	(01 - 09) Aeronautics: (08) Aircraft Stability And Control Aircraft/Project: F-18 AFF
ID Code:	20
Deposited On:	28 May 2004
Additional Information:	33 pages.