Attaining Optimal Autorotative Profiles Using Active Inceptor Cueing

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-10-C-0070
Agency Tracking Number: N093-165-0928
Amount: $79,999.00
Phase: Phase I
Program: SBIR
Awards Year: 2010
Solicitation Year: 2009
Solicitation Topic Code: N093-165
Solicitation Number: 2009.3
Small Business Information
2 Trap Falls Rd, Suite 204, Shelton, CT, 06484
DUNS: 793503819
HUBZone Owned: N
Woman Owned: Y
Socially and Economically Disadvantaged: N
Principal Investigator
 Naji Yakzan
 Engineering Manager
 (203) 926-2722
Business Contact
 Linda Yakzan
Title: President
Phone: (714) 488-0100
Email: linda.s.yakzan@newenglandanalyticsl
Research Institution
As modern helicopters get heavier and their rotors get lighter, the odds of a successful outcome from an engine failure diminish. Previous research has demonstrated that for every point on the height velocity aircraft envelope there exists an optimal autorotative profile. While the optimal profile does not guarantee a successful landing, it does increase the chances of one. New England Analytics believes that through the use of active control inceptors, the aircraft can be flown to the optimal profile. The active inceptors will provide cues to the pilot indicating the required control inputs to achieve the optimal profile. To determine the optimal cues, NEA will conduct a survey of available tactile cues and assess those cues as to their functionality in assisting the pilot attain the optimum profile. The survey will look at tactile cues for use on both the collective and pitch cyclic. Additionally, NEA will examine the various inceptor configurations so as to ensure that the cues determined as optimal are effective across the various configurations. Finally, NEA will develop a conceptual tactile cueing design for the CH-53K.

* Information listed above is at the time of submission. *

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