Investigation Of Hardware-In-Loop Simulation (HILS) For Guidance System

摘要：

　　Flight motion simulator (FMS) is a high-bandwidth angular motion system for the simulation of missile dynamics.This paper describes the initial laboratory integration of the hardware-in-loop Simulation (HILS) for homing guided missile system.HILS facilities and methodology form an integrated system for transforming a preliminary guidance and control system design to flight software and hardware from initial launching till impact.FMS will be driven by the output of deterministic simulations and will replicate the time history of the command signals.This paper describes the motivation,the servo system,mechanical,and electronic subsystems,and control software and algorithms.Moreover,the software user interfaces for the FMS.Six-degrees-of-freedom (6-DOF) flying body model is utilized in association with graphical user interface (GUI) for FMS.

关键词： HILS Missile Seeker

作者: Adel Alsaraj Gene Stuffle

作者单位: Electrical Engineering Department Idaho State University Pocatello, Idaho

会议类型: 国际会议

会议名称: 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference(IAEAC 2015)(2015 IEEE先进信息技术,电子与自动化控制国际会议)

会议地点: 重庆

会议语种:英文

页码: 704-708

在线出版日期: 2015-12-19（万方平台首次上网日期，不代表论文的发表时间）