Piloted Full-Motion Simulation with Simulink®

Lewis, Emily K

关键词: VERTICAL MOTION SIMULATORS;    IN-FLIGHT SIMULATION;    MATHEMATICAL MODELS;    REAL TIME OPERATION;    COMPUTER PROGRAMS;    COMPUTERIZED SIMULATION;    FLIGHT CONTROL;    TEST PILOTS;    ROTARY WING AIRCRAFT;    HELICOPTER DESIGN;    HARDWARE-IN-THE-LOOP SIMULATION;    RESEARCH FACILITIES;   

RP-ID  :  ARC-E-DAA-TN64603,ARC-E-DAA-TN63713

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

A recent experiment at NASA Ames Research Center’s Vertical Motion Simulator (VMS) successfully combined a real-time, human in-the-loop architecture with the flexibility of operating in the Simulink® graphical model-based engineering environment. The VMS is a large amplitude flight simulator designed to be adaptable to provide rapid integration and development of a wide variety of vehicles and support diverse aeronautical investigations. Math models are often programmed in Simulink. Typically, to run Simulink models in real time, they are converted to C code. However, the conversion and integration process can be time consuming and cumbersome. Thus, the VMS facility capabilities were expanded to allow a Simulink vehicle math model to run in the MathWorks’ MATLAB environment during a piloted full-motion simulation experiment. The MATLAB Simulink based approach to driving the VMS was found to decrease development time by allowing quick integration of math model changes and providing the ability to run the same version of the model on researcher’s desktop computers. This accomplishment demonstrated that the development ease of the graphical Simulink environment could be retained, while working within the real-time environment of the VMS architecture and maintaining the unique flexibility of the VMS.