案例式“航天器大角度机动”全物理仿真实验设计与实践  

Design and practice of case-based “Spacecraft large angle maneuver” physical simulation experiment

作　　者：刘睿[1] 周军[1] 刘莹莹[1] 郭建国[1] LIU Rui;ZHOU Jun;LIU Yingying;GUO Jianguo(National Joint Engineering Laboratory for Micro-Satellite Technology and Application,Northwestern Polytechnical University,Xi’an 710072,China)

机构地区：[1]西北工业大学微小卫星技术及应用国家和地方联合工程实验室,陕西西安710072

出　　处：《实验技术与管理》2021年第4期210-213,共4页Experimental Technology and Management

基　　金：陕西省新工科研究与实践项目(20GZ110102);西北工业大学研究生实践能力提升计划项目(20GH010201);西北工业大学教育教学改革研究项目(20200023)。

摘　　要：飞行器控制系统是航天控制类专业的基础核心课程,实践性很强。文章针对航天器应用背景,设计了基于全物理仿真的航天器大角度机动实验案例,使之成为课程理论教学与工程实践之间的桥梁。文章对引导学生根据航天器姿态控制需求分析解决实际问题、运用课程理论知识设计控制律并进行实验验证的具体做法进行了介绍,是对案例式实验教学的有益探索。Aircraft control system is the basic course of aerospace control specialty, which is highly practical. Aiming at the application background of spacecraft, this paper designs a spacecraft large angle maneuver experiment case based on full physical simulation, which makes it a bridge between theoretical teaching and engineering practice, and introduces how to guide students to analyze and solve practical problems according to spacecraft attitude control requirements, and how to design control law by using theoretical knowledge of the course and carry out experimental verification, which is a beneficial exploration of case-based experimental teaching.

关 键 词：案例教学法 航天器控制 实验教学 全物理仿真 

分 类 号：G642.0[文化科学—高等教育学]