Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Vineet Sahasrabudhe"'
Autor:
Kenny K. Cheung, Sean Shan-Min Swei, Christopher L. Blanken, Alexander Faynberg, Mark B. Tischler, Vineet Sahasrabudhe
Publikováno v:
Journal of Guidance, Control, and Dynamics. 28:964-978
Modernized control laws were developed to provide an attitude-command/attitude-hold response type for the UH-60 BLACK HAWK helicopter and thereby afford improved handling qualities for near-Earth operation in night and poor weather. The inner-loop sy
Autor:
Roberto Celi, Vineet Sahasrabudhe
Publikováno v:
Journal of Aircraft. 34:730-739
This paper describes a new technique for the calculation of gradients of constraints associated with the moderate amplitude criteria of the ADS-33 helicopter handling qualities specifications. The gradients are calculated using low-order linear appro
Publikováno v:
Journal of Guidance, Control, and Dynamics. 20:217-224
The results are presented of a study concerning the integrated optimization of rotor and e ight control systems with simultaneousaeroelastic and handling qualitiesconstraints. Arepresentative subset of theADS-33C handling qualities specie cation isre
Publikováno v:
Proceedings of the 2010 American Control Conference.
Constraint reduction has been proposed, in the context of linear and quadratic primal-dual interior-point optimization, as an approach for efficiently handling problems in which the number of inequality constraints far exceeds that of decision variab
Publikováno v:
Atmospheric Flight Mechanics Conference.
The use of an Automatic Flutter-suppression System (AFS) increases the challenge of flutter flight-testing because the aircraft is required to fly in a region where it is open loop unstable. Paradoxically, the presence of the AFS can be exploited to
Publikováno v:
37th Aerospace Sciences Meeting and Exhibit.
Autor:
Anshu Mehra, Vineet Sahasrabudhe
Publikováno v:
Guidance, Navigation, and Control Conference and Exhibit.
In this paper, we present the control of smart structures using a multi-agent control paradigm as a new option for aircraft active control that promotes the efficient integration of vehicle and structural dynamics with the control system. We first de
Publikováno v:
SPIE Proceedings.
Vibration and noise are two long-standing problems that have limited the expansion of military and commercial applications of rotorcraft. The source of these interrelated phenomena is the main rotor, which operates in an unsteady and complex aerodyna
Publikováno v:
Journal of the American Helicopter Society. 51:215
Conference
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