Zobrazeno 1 - 10
of 30
pro vyhledávání: '"D. Gangsaas"'
Autor:
Q. Mendoza, Charles R. Porter, N. Albion, J. Folky, D. Gangsaas, Chi-Shain Hong, Luis Figueroa
Publikováno v:
LEOS 1991 Summer Topical Meetings on Spaceborne Photonics: Aerospace Applications of Lasers and Electro-Optics, Optical Millimeter-Wave Interactions: Measurements, Generation, Transmission and Control.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::242e7466dfed1a12941d9b6f087d97fc
https://doi.org/10.1109/leosst.1991.665231
https://doi.org/10.1109/leosst.1991.665231
Autor:
Quinn Mendoza, Luis Figueroa, N. Albion, Charles R. Porter, John N. Polky, D. Gangsaas, Chi-Shain Hong
Publikováno v:
Integrated Optoelectronics for Communication and Processing.
N. Albion, L. Figueroa, C. S. Hong, 0. Gangsaas,0. Mendoza, J. Polky, and C. PorterBoeing Defense & Space GroupP0 Box 3999, M/S 7J-05Seattle, WA 98124-2499(206) 865-3135Over the last several years, it has become widely recognized that electromagnetic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8604ed2a51b1a203759134b11bc2002f
https://doi.org/10.1117/12.134997
https://doi.org/10.1117/12.134997
Publikováno v:
Journal of Guidance, Control, and Dynamics. 9:546-554
The synthesis of a command and stability augmentation control law for a transport airplane is presented. To improve fuel efficiency, the airplane has a relatively small horizontal tail surface and therfore has unsatisfactory inherent longitudinal sta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7476168f5e9c1237b3f7e8146f802b5c
https://doi.org/10.2514/3.20145
https://doi.org/10.2514/3.20145
Publikováno v:
IFAC Proceedings Volumes. 15:1359-1364
Flutter mode control is critical for flexible wing aircraft designed for fuel efficiency. However, parameters associated with the unstable flutter may only be imprecisely calculated from sensor data, and classical or modern controllers which of neces
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f5f816230df2a8b15e958b0b7fbb862a
https://doi.org/10.1016/s1474-6670(17)63187-2
https://doi.org/10.1016/s1474-6670(17)63187-2
Publikováno v:
IEEE Transactions on Automatic Control. 31:995-1014
The role of feedback control in the solution of aircraft stability and control problems is discussed. It is argued that this role is becoming more and more important and is a key to meeting performance objectives for new aircraft. As a consequence, t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::561d50281fab3d7005fc283c1dbeb79b
https://doi.org/10.1109/tac.1986.1104161
https://doi.org/10.1109/tac.1986.1104161
Publikováno v:
IFAC Proceedings Volumes. 18:345-349
This paper presents the application of adaptive control to flutter suppression on a flexible aircraft. The adaptive control law is integrated with a nominal constant gain controller and furnishes the equivalent of a 180 0 phase margin at the flutter
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3279dcf94f65e7787e05f2669d7a65da
https://doi.org/10.1016/s1474-6670(17)60583-4
https://doi.org/10.1016/s1474-6670(17)60583-4
Publikováno v:
Aircraft Design, Systems and Technology Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::12ead7e085d5158e97175d31d864db57
https://doi.org/10.2514/6.1983-2560
https://doi.org/10.2514/6.1983-2560
Autor:
D. Gangsaas, J. D. Blight
Publikováno v:
19th Aerospace Sciences Meeting.
A speed-hold system for an experimental short takeoff and landing jet airplane has been designed using both classical root-locus and modern optimal control synthesis techniques. The purpose of the speed-hold system is to maintain airspeed during fina
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd7fd0b718339cce309a3b027506ec26
https://doi.org/10.2514/6.1981-17
https://doi.org/10.2514/6.1981-17
Development and Evaluation of Integrated Flight/Propulsion Control Algorithms for a Tactical Fighter
Publikováno v:
Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery.
Linear quadratic synthesis is applied to the design of an integrated vertical flight path and airspeed command and stability augmentation control law for the AFTI/F-111 aircraft. A feedforward controller combined with full-state feedback provides nea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5283e0684e3662b8b736dec75035891
https://doi.org/10.1115/84-gt-282
https://doi.org/10.1115/84-gt-282
Publikováno v:
19th Aerospace Sciences Meeting.
A modified linear quadratic Gaussian (LQG) synthesis procedure has been used to design low-order robust multiloop controllers for a flexible airplane. The introduction of properly constructed fictitious Gauss-Markov processes in the control loops all
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b3690ef92a4e15f525bcad8d16c6b715
https://doi.org/10.2514/6.1981-21
https://doi.org/10.2514/6.1981-21