Nasa Aircraft Controls Research 1983

Author : National Aeronautics and Space Administration (NASA)
Publisher :
ISBN 13 : 9781466499676
Total Pages : 32 pages
Book Rating : 4.4/5 (996 download)

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Download or read book Assessment of the State of the Art of Flight Control written by National Aeronautics and Space Administration (NASA) and published by . This book was released on 2010-11-01 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: A survey of literature from academia, industry, and other Government agencies was reviewed to assess the state of the art in flight control technologies as related to the identified adverse conditions. A general state of the art in adaptive flight control is summarized first, followed by an assessment of the state of the art as applicable to 13 identified adverse conditions. The state-of-the-art summaries include technologies not specifically related to flight control, but may serve as inputs to a future flight control algorithm. The adverse conditions were determined as a result of a previous study and can be found in NASA Technical Memorandum entitled "Causal Factors and Adverse Conditions of Aviation Accidents and Incidents Related to Integrated Resilient Aircraft Control." The types of adverse conditions are divided into three separate groups: failure of aircraft system or component, damage to a structure or component, and control upsets related to pilot error or another cause that cannot be regulated by aircraft technology. In general, there were two distinct methods for implementing adaptive flight control systems. In the first method, the system assists the pilot in operating the aircraft in a degraded state by providing additional information on the degradation state of the aircraft and then makes calculations relating to alternative use of controls or alternative maneuvers. The second type of implementation involves no change in the pilot's method of operation in relation to a nominal operating environment. The adaptive control system takes the nominal control inputs given by the pilot, performs calculations based on the degradation state of the aircraft, and sends alternative commands to the vehicle control surfaces and/or propulsion system. This method is very different than the first, as the pilot is not required to alter the operation of the plane due to the degradation. Much more research is being done on failures and degradation of specific components in relation to adaptive control systems. Although component research is important, as it can provide better input data into adaptive control systems, more can be done to advance the state of the art of the actual adaptive control systems. In regards to the two methods of implementing adaptive control, the trend is that the state of the art is moving in the direction of systems in which the pilot operates the aircraft the same in both nominal and off-nominal conditions where the adaptive control system itself alters the commands that go to the control surfaces and propulsion system when operating in an off-nominal state.