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检索条件"主题词=Flight Test Programme"
152 条 记 录,以下是11-20 订阅
排序:
Evaluation of an L1 Adaptive flight Control Law on Calspan's Variable-Stability Learjet
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2017年 第4期40卷 1050-1059页
作者: Ackerman, Kasey A. Xargay, Enric Choe, Ronald Hovakimyan, Naira Cotting, M. Christopher Jeffrey, Robert B. Blackstun, Margaret P. Fulkerson, T. Paul Lau, Timothy R. Stephens, Shawn S. Univ Illinois Dept Mech Sci & Engn Urbana IL 61801 USA Univ Illinois Dept Mech Sci & Engn Urbana IL 61801 USA US Air Force Test Pilot Sch Flying Qual Edwards AFB CA 93524 USA US Air Force Test Pilot Sch Edwards AFB CA 93524 USA
A study presented flight-test results of a variable-stability Learjet aircraft augmented with an L1 adaptive flight control law. The flight tests were conducted by the US Air Force (USAF) test Pilot School (TPS) at Ed... 详细信息
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Adaptive Glide Slope Control for Parafoil and Payload Aircraft
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2013年 第4期36卷 1019-1034页
作者: Ward, Michael Costello, Mark Georgia Inst Technol Guggenheim Sch Aerosp Engn Atlanta GA 30332 USA Georgia Inst Technol Guggenheim Sch Aerosp Engn Woodruff Sch Mech Engn Atlanta GA 30332 USA
The invention of the steerable, gliding, ram-air parafoil enabled the possibility of precision, autonomous aerial payload delivery. Research and development work on guided airdrop systems has focused primarily on evol... 详细信息
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BANK-TO-TURN MISSILE AUTOPILOT DESIGN USING LOOP TRANSFER RECOVERY
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1990年 第1期13卷 145-152页
作者: WISE, KA SO ILLINOIS UNIV ELECT ENGNEDWARDSVILLEIL 62026
Linear quadratic Gaussian/loop transfer recovery control theory is used to design a bank-to-turn missile autopilot. This paper presents the steps of the design and analysis procedure and demonstrates them in designing... 详细信息
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PRACTICAL flight test METHOD FOR DETERMINING RECIPROCATING-ENGINE COOLING REQUIREMENTS
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JOURNAL OF AIRCRAFT 1984年 第12期21卷 936-942页
作者: WARD, DT MILEY, SJ Texas A&M University College Station Texas
A practical flight test procedure has been developed and verified for determining the cooling requirements for an installed air cooled reciprocating engine of any type The technique is based on a simple modification o... 详细信息
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COMPUTATIONAL REQUIREMENTS FOR HYPERSONIC flight PERFORMANCE ESTIMATES
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JOURNAL OF SPACECRAFT AND ROCKETS 1990年 第2期27卷 103-112页
作者: MEHTA, UB NASA Ames Research Center Moffett Field California 94035
Among the many new hypervelocity vehicles being considered for development, the air breathing, single stage-to-orbit transatmospheric vehicles and aeroassisted orbital-transfer vehicles are going to be designed largel... 详细信息
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flight test OF THE JAPANESE UPPER SURFACE BLOWING STOL EXPERIMENTAL AIRCRAFT ASKA
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JOURNAL OF AIRCRAFT 1991年 第10期28卷 630-637页
作者: YAMATO, H OKADA, N BANDO, T University of Tokyo Tokyo Japan National Aerospace Laboratory Tokyo Japan
The Upper Surface Blowing STOL aircraft named ASKA was developed and flight tested by the National Aerospace Laboratory of Japan between 1977-1989. The aircraft was a conversion of the Kawasaki C-1 medium transport, w... 详细信息
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WIND PROFILE MEASUREMENT USING LIFTING SENSORS
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JOURNAL OF SPACECRAFT AND ROCKETS 1966年 第3期3卷 365-&页
作者: STENGEL, RF Princeton University Princeton N. J.
A vertical profile of wind velocity for use in rocket prelaunch operations should be measured rapidly in order to minimize the space-time displacement between the measured profile and the ascent trajectory. A lifting ... 详细信息
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REAL-TIME COMPARISON OF X-29A flight DATA AND SIMULATION DATA
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JOURNAL OF AIRCRAFT 1989年 第2期26卷 117-123页
作者: BAUER, JE CRAWFORD, DB GERA, J ANDRISANI, D Purdue University West Lafayette Indiana NASA Ames Research Center Edwards California
This paper presents a technique for comparing, in real time, the flight-test time histories for X-29A aircraft with time histories computed from linearized mathematical models. Such a comparison allows the flight-test... 详细信息
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SCATTERING PROPERTIES OF ICE PARTICLES FORMED BY RELEASE OF H2O IN VACUUM
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JOURNAL OF SPACECRAFT AND ROCKETS 1974年 第1期11卷 54-56页
作者: KASSAL, TT GRUMMAN AEROSP CORP BETHPAGENY 11714
The scattering characteristics of an aggregate of ice particles formed by injecting a stream of water into a vacuum tank were determined experimentally. Although the experiments were performed in the absence of solar ... 详细信息
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Current Methods Modeling and Simulating Icing Effects on Aircraft Performance, Stability, Control
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JOURNAL OF AIRCRAFT 2010年 第1期47卷 201-211页
作者: Ratvasky, Thomas P. Barnhart, Billy P. Lee, Sam NASA John H Glenn Res Ctr Lewis Field Icing Branch Cleveland OH 44135 USA Bihrle Appl Res Inc Hampton VA 23666 USA ASRC Aerosp Corp Icing Branch Cleveland OH 44135 USA
Icing alters the shape and surface characteristics of aircraft components, which results in altered aerodynamic forces and moments caused by air flow over those iced components. The typical effects of icing are increa... 详细信息
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