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A High-Fidelity Batch Simulation Environment for Integrated Batch and Piloted Air Combat Simulation AnalysisA batch air combat simulation environment known as the Tactical Maneuvering Simulator (TMS) is presented. The TMS serves as a tool for developing and evaluating tactical maneuvering logics. The environment can also be used to evaluate the tactical implications of perturbations to aircraft performance or supporting systems. The TMS is capable of simulating air combat between any number of engagement participants, with practical limits imposed by computer memory and processing power. Aircraft are modeled using equations of motion, control laws, aerodynamics and propulsive characteristics equivalent to those used in high-fidelity piloted simulation. Databases representative of a modern high-performance aircraft with and without thrust-vectoring capability are included. To simplify the task of developing and implementing maneuvering logics in the TMS, an outer-loop control system known as the Tactical Autopilot (TA) is implemented in the aircraft simulation model. The TA converts guidance commands issued by computerized maneuvering logics in the form of desired angle-of-attack and wind axis-bank angle into inputs to the inner-loop control augmentation system of the aircraft. This report describes the capabilities and operation of the TMS.
Document ID
20040129590
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Goodrich, Kenneth H.
(NASA Langley Research Center Hampton, VA, United States)
McManus, John W.
(NASA Langley Research Center Hampton, VA, United States)
Chappell, Alan R.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1992
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA Paper 92-4145
Report Number: AIAA Paper 92-4145
Distribution Limits
Public
Copyright
Public Use Permitted.
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