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  • 1
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    Lateral directional control characteristics (1961)
    In:  CASI
    Details
    Publication Date: 2004-12-22
    Keywords: unknown
    Type: RES.-AIRPLANE-COMM. REPT. ON CONF. ON THE PROGR. OF THE X-15 PROJ. 1961; P 131-154
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Status and trends in active control technology (1975)
    In:  CASI
    Details
    Publication Date: 2006-01-11
    Description: The emergence of highly reliable fly-by-wire flight control systems makes it possible to consider a strong reliance on automatic control systems in the design optimization of future aircraft. This design philosophy has been referred to as the control configured vehicle approach or the application of active control technology. Several studies and flight tests sponsored by the Air Force and NASA have demonstrated the potential benefits of control configured vehicles and active control technology. The present status and trends of active control technology are reviewed and the impact it will have on aircraft designs, design techniques, and the designer is predicted.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Type: NASA/Univ. Conf. on Aeron.; p 273-322
    Format: text
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  • 3
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    An overview of parameter estimation techniques and applications in aircraft flight testing (1974)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: Parameter estimation is discussed as it applies to aircraft flight testing, and an overview of the symposium is presented. The evolution of techniques used in flight testing is reviewed briefly, and it is pointed out how the changing character of the aircraft tested and the availability of advanced data systems have promoted this evolution. Recent advances in optimal estimation theory have stimulated widespread interest and activity in parameter estimation. The framework of these advanced techniques is outlined to set the stage for subsequent papers. The session topics are introduced and related to the requirements of flight-test research.
    Keywords: AIRCRAFT
    Type: Parameter Estimation Tech. and Appl. in Aircraft Flight Testing; p 1-18
    Format: text
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  • 4
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    FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES OF A SUPERSONIC AIRPLANE WITH A LOW-ASPECT-RATIO UNSWEPT WING AND A TEE-TAIL (1959)
    In:  CASI
    Details
    Publication Date: 2019-05-11
    Description: Flight-determined stability & control derivatives of supersonic aircraft with low aspect ratio unswept wing & t-tail
    Keywords: BIOSCIENCES
    Type: NASA-MEMO-2-2-59H
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    An advanced method for airborne simulation (1964)
    In:  CASI
    Details
    Publication Date: 2019-05-22
    Description: Advanced aircraft simulator for pilot training
    Keywords: ELECTRONICS
    Type: NASA-RP-337
    Format: text
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    NASA TECHNICAL REPORTS
  • 6
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    Technology review of flight crucial flight control systems (application of optical technology) (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The survey covers the various optical elements that are considered in a fly-by-light flight control system including optical sensors and transducers, optical data links, so-called optical actuators, and optical/electro-optical processing. It also addresses airframe installation, maintenance, and repair issues. Rather than an in-depth treatment of optical technology, the survey concentrates on technology readiness and the potential advantages/disadvantages of applying the technology. The information was assembled from open literature, personal interviews, and responses to a questionnaire distributed specifically for this survey. Not all of the information obtained was consistent, particularly with respect to technology readiness. The synthesis of information into the perception of the state-of-technology is presented.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Type: NASA-CR-172332-SUPPL-1 , NAS 1.26:172332-SUPPL-1
    Format: application/pdf
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  • 7
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    Lateral-directional control of the x-15 airplane (1962)
    In:  CASI
    Details
    Publication Date: 2019-05-23
    Description: Lateral directional control and stability characteristics of X-15 aircraft
    Keywords: AIRCRAFT
    Type: NASA-TM-X-726
    Format: application/pdf
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  • 8
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    Foreign technology summary of flight crucial flight control systems (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A survey of foreign technology in flight crucial flight controls is being conducted to provide a data base for planning future research and technology programs. Only Free World countries were surveyed, and the primary emphasis was on Western Europe because that is where the most advanced technology resides. The survey includes major contemporary systems on operational aircraft, R&D flight programs, advanced aircraft developments, and major research and technology programs. The information was collected from open literature, personal communications, and a tour of several companies, government organizations, and research laboratories in the United Kingdom, France, and the Federal Republic of Germany. A summary of the survey results to date is presented.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Type: NASA. Langley Research Center NASA Aircraft Controls Research, 1983; p 365-386
    Format: application/pdf
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  • 9
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    Technology review of flight crucial flight controls (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The results of a technology survey in flight crucial flight controls conducted as a data base for planning future research and technology programs are provided. Free world countries were surveyed with primary emphasis on the United States and Western Europe because that is where the most advanced technology resides. The survey includes major contemporary systems on operational aircraft, R&D flight programs, advanced aircraft developments, and major research and technology programs. The survey was not intended to be an in-depth treatment of the technology elements, but rather a study of major trends in systems level technology. The information was collected from open literature, personal communications and a tour of several companies, government organizations and research laboratories in the United States, United Kingdom, France, and the Federal Republic of Germany.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Type: NASA-CR-172332 , NAS 1.26:172332 , HR-78500037
    Format: application/pdf
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  • 10
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    A new model performance index for the engineering design of flight control systems. (1969)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Model performance index /PI/ providing criterion for approximating one dynamic flight control system by another based on geometrical representation of linear autonomous systems
    Keywords: NAVIGATION
    Type: AIAA PAPER 69-885 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, GUIDANCE, CONTROL, AND FLIGHT MECHANICS CONFERENCE; Aug 18, 1969 - Aug 20, 1969; PRINCETON, NJ
    Format: text
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