Results 101 to 110 of about 5,164 (216)
Flight control systems properties and problems, volume 1 [PDF]
This volume contains a delineation of fundamental and mechanization-specific flight control characteristics and problems gleaned from many sources and spanning a period of over two decades.
Johnston, D. E., Mcruer, D. T.
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Multi-axis transient vibration testing of space objects: Test philosophy, test facility, and control strategy [PDF]
IABG has been using various servohydraulic test facilities for many years for the reproduction of service loads and environmental loads on all kinds of test objects.
Lachenmayr, Georg
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Application of active control landing gear technology to the A-10 aircraft [PDF]
Two concepts which reduce the A-10 aircraft's wing/gear interface forces as a result of applying active control technology to the main landing gear are described.
Edson, R., Ross, I.
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Proceedings of the JFPS International Symposium on Fluid Power, 1993 Shinichi YOKOTA +2 more
openaire +3 more sources
Automated mixed traffic vehicle design AMTV 2 [PDF]
The design of an improved and enclosed Automated Mixed Traffic Transit (AMTT) vehicle is described. AMTT is an innovative concept for low-speed tram-type transit in which suitable vehicles are equipped with sensors and controls to permit them to operate ...
Cassell, P. L. +2 more
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An analog computer study of hydraulic servomechanism nonlinearlities [PDF]
, 1954 Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1954.Includes bibliographical references (p. 105-106).by Keith A. Erikson, William R. Greenwood, Philip J.
Bonomo, Philip J +2 more
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Development of a general purpose airborne simulator [PDF]
Variable stability system development for General Purpose Airborne Simulator ...
Arendt, R. H. +2 more
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Ultrasonically bonded value assembly [PDF]
, 1975 A valve apparatus capable of maintaining a fluid-tight seal over a relatively long period of time by releasably bonding a valve member to its seat is described.
Salvinski, R. J.
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An electric control for an electrohydraulic active control aircraft landing gear [PDF]
An electronic controller for an electrohydraulic active control aircraft landing gear was developed. Drop tests of a modified gear from a 2722 Kg (6000 lbm) class of airplane were conducted to illustrate controller performance.
Edson, R., Ross, I.
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Research of Power Balance of Belt Conveyor Driven by Multi-motor and Its Analysis
Gong-kuang zidonghua, 2011 For belt conveyor driven by multi-motor, the problem of multi-motor power balance must be paid attention to for preventing equipments from being destroyed by unbalanced loading on individual motor.
XU Lu-hui +4 more
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