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Visualized Flight Control and Flight Mechanics Calculation
Abstract:
Aircraft basic performance is the foundation of the research on aircraft, which is characterized by many parameters. According to the example of the shortest rising time spent on flying from an altitude to another arbitrary one, and the example of matching control of joystick and throttle lever, it is demonstrated that the visualization in scientific computing method is useful for promoting engineering research.
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Pages:
759-762
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Online since:
August 2012
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© 2012 Trans Tech Publications Ltd. All Rights Reserved
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