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Synonyme wurden verwendet für: FLIGHT • VEHICLE
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1–20 von 444 Ergebnissen

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Hypersonic flight: the need for a new legal regime

Schwetje, F.K. / Walsh, D.E. | Tema Archiv | 1989

Schlagwörter: HYPERSONIC FLIGHT , TRANS ATMOSPHERIC VEHICLE

A rapid prototyping facility for flight research in advanced systems concepts

Duke, E.L. / Brumbaugh, R.W. / Disbrow, J.D. | Tema Archiv | 1989

Schlagwörter: FLIGHT RESEARCH , DRYDEN FLIGHT RESEARCH FACILITY , REMOTELY AUGMENTED VEHICLE

The STOL maneuver technology demonstrator manned simulation test program

Feeser, K.A. / Zeh, J.M. / Leggett, D.B. | Tema Archiv | 1989

Schlagwörter: PILOT-VEHICLE INTERFACE , OPERATIONAL FLIGHT PROGRAM CONTROL LAWS

Transfer orbit stage gyrocompass alignment algorithm twist and sway environment for Mar's Observer mission on commercial Titan

Reddy, N.S. / Murray, J. | Tema Archiv | 1991

Schlagwörter: BOOSTER VEHICLE , EXPANDABLE LAUNCH VEHICLE , FLIGHT COMPUTER

INTELSAT-K launch vehicle considerations

Goldman, A.M. jun. / Ozkul, A. | Tema Archiv | 1995

Schlagwörter: Intelsat-K launch vehicle , Atlas II-A launch vehicle , flight performance

Control and guidance of a UMA using GPS

Dyer, D.J. / Lewis, D.J.G. / Stevenson, A. | IET Digital Library Archive | 1995

Schlagwörter: data-gathering flight trials , digital flight control system , flight testing , XRAE1 air vehicle

Performance enhancement of a multiple model adaptive estimator

Maybeck, P.S. / Hanlon, P.D. | Tema Archiv | 1995

Schlagwörter: unmanned flight vehicle

Closing all the loops

Gillespie, A.R. | IET Digital Library Archive | 1998

Schlagwörter: low-level flight , flight path , integrated vehicle management system

A flight control design of a re-entry vehicle using a double-loop control system with fuzzy gain-scheduling

Fujimori, A / Nikiforuk, P N / Gupta, M M | SAGE Publications | 2001

Schlagwörter: re-entry vehicle , flight control

Application of NDI flight control to a second generation supersonic transport aircraft

Steer, A.J. | IET Digital Library Archive | 2001

Schlagwörter: NDI flight control , vehicle dynamic model , flight envelope , fly-by-wire flight control system

Preliminary design and wind tunnel tests of a micro air vehicle for surveillance and sensor-bearing applications

La Rosa, G / Mirone, G / Risitano, A | SAGE Publications | 2005

Schlagwörter: micro air vehicle , low Reynolds flight

System identification and 6-DOF hovering controller design of unmanned model helicopter

Kim, Byeongil / Chang, Yushin / Lee, Man Hyung | Tema Archiv | 2006

Schlagwörter: RUAV (Rotorcraft-based Unmanned Aerial Vehicle) , Fliegen

Design of the flight management system for a shrouded-fan uninhabited aerial vehicle

Avanzini, G / de Matteis, G | SAGE Publications | 2006

Schlagwörter: flight management system , uninhabited aerial vehicle

Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: Implementation and validation

Ansari, S A / Żbikowski, R / Knowles, K | SAGE Publications | 2006

Schlagwörter: micro-air vehicle design , insect flight

Ultra-lightweight synthetic aperture radar based on a 35 GHz FMCW sensor concept and online raw data transmission

Edrich, M. | IET Digital Library Archive | 2006

Schlagwörter: unmanned aerial vehicle , test flight

Power balance method in calculation of helicopter maneuverability taking into account specific operational conditions

Mikhailov, S. A. / Onushkin, A. Yu. | Springer Verlag | 2007

Schlagwörter: Flight Speed , Flight Vehicle

Power balance method in calculation of helicopter maneuverability taking into account specific operational conditions

Mikhailov, S. A. / Onushkin, A. Yu. | Online Contents | 2007

Schlagwörter: Flight Vehicle , Flight Speed

Coefficients of equilibrium equations in solving a problem of reconstructing deformation curves for slightly conical thin-walled structures

Kostin, V. A. / Valitova, N. L. | Springer Verlag | 2007