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A High-Fidelity Batch Simulation Environment for Integrated Batch and Piloted Air Combat Simulation Analysis

机译:高保真批处理仿真环境,用于批处理和空战综合仿真分析

摘要

A 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.
机译:提出了一种称为战术机动模拟器(TMS)的批量空战模拟环境。 TMS可作为开发和评估战术机动逻辑的工具。该环境还可以用于评估扰动对飞机性能或支持系统的战术影响。 TMS能够模拟任意数量的参与人员之间的空战,而计算机存储和处理能力会带来实际限制。使用运动方程,控制律,空气动力学和推进特性对飞机进行建模,这些方程等效于高保真飞行员模拟中使用的方程。包括代表具有和不具有推力矢量功能的现代高性能飞机的数据库。为了简化在TMS中开发和实施操纵逻辑的任务,在飞机仿真模型中实施了称为战术自动驾驶仪(TA)的外环控制系统。 TA将由计算机操纵逻辑发出的,以所需攻角和风轴倾斜角形式的制导命令转换为飞机内环控制增强系统的输入。该报告描述了TMS的功能和操作。

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