Intelligent Architecture and Hybrid Model of Ground and Launch System for Advanced Launch Site

被引:0
|
作者
Xiao, Litian [1 ]
Xiao, Nan [2 ]
Li, Mengyuan [1 ]
Liu, Zhanqing [1 ]
Wang, Fei [1 ]
Li, Yuliang [1 ]
Hou, Kewen [1 ]
机构
[1] Beijing Special Engn Design & Res Inst, POB 4702, Beijing 100028, Peoples R China
[2] China Aerosp Acad Syst Sci & Engn, 8 Fucheng Rd, Beijing 100048, Peoples R China
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper proposes an intelligent functional architecture for an advanced launch site system that is composed of five parts: the intelligent technical area, the intelligent launching region, the intelligent flight and landing area, the intelligent command and control system, and the intelligent analysis assessment system. The five parts consist of the infrastructure, facilities, equipment, hardware and software and thus include the whole mission processes of ground and launch systems from flight articles' entry to launch. The architectural framework is designed for the intelligent elements of the parts. The framework is also defined as the interrelationship and the interface of the elements, including the launch vehicle and flight payloads. Based on the Internet of Things (IoT), the framework is integrated on four levels: the physical layer, the perception layer, the network layer, and the application layer. The physical layer includes the physical objects and actuators of the launch site. The perception layer consists of the sensors and data processing system. The network layer supplies the access gateways and backbone network. The application layer serves application systems through the middleware platform. The core of the intelligent system is the controller of the automatic control system crossing the four layers. This study builds the models of the IoT, cloud platform, middleware, integrated access gateway, and automatic control system for actual ground and launch systems. A formal approach describes and defines the architecture, models and autonomous control flows in the paper. The defined models describe the physical objects, intelligent elements, interface relations, status transformation functions, etc. The test operation and launch processes are connected with the intelligent system model. This study has been applied to an individual mission project and achieved good results. The architecture and the models of this study regulate the relationship between the elements of the intelligent system. The study lays a foundation for the architectural construction, the simulation and the verification of the intelligent systems at the launch site.
引用
收藏
页数:12
相关论文
共 50 条
  • [1] Evolution of the Florida Launch Site Architecture, Enhancing Launch Opportunities
    Gray, James
    Colloredo, Scott
    [J]. 2012 IEEE AEROSPACE CONFERENCE, 2012,
  • [2] An Architecture of FPGA-Based Controller on Automatic Control System for Test and Launch in Launch Site
    Xiao, Litian
    Wang, Weiguo
    Hou, Kewen
    Li, Mengyuan
    Wang, Fei
    Li, Yuliang
    [J]. PROCEEDINGS OF THE 2ND INTERNATIONAL CONFERENCE ON COMPUTER SCIENCE AND APPLICATION ENGINEERING (CSAE2018), 2018,
  • [3] Remote Intelligent Support Architecture for Ground Equipment Control in Space Launch Sites
    Xiao, Litian
    Li, Mengyuan
    Hou, Kewen
    Wang, Fei
    Li, Yuliang
    [J]. ADVANCES IN HARMONY SEARCH, SOFT COMPUTING AND APPLICATIONS, 2020, 1063 : 226 - 234
  • [4] THE ADVANCED LAUNCH SYSTEM (ALS)
    ELDRED, CH
    [J]. CASE FOR MARS 111 : STRATEGIES FOR EXPLORATION - TECHNICAL, 1989, 75 : 349 - 354
  • [5] Hybrid launch isolation system
    Sciulli, D
    Griffin, SF
    [J]. SMART STRUCTURES AND MATERIALS 1999: INDUSTRIAL AND COMMERCIAL APPLICATIONS OF SMART STRUCTURES TECHNOLOGIES, 1999, 3674 : 352 - 359
  • [6] Integrated Design and Implementation of Ground Test Launch and Control System of Advanced Upper Stage for New Generation Launch Vehicle
    Cai Yuanwen
    Xie Weiqi
    Yao Jingbo
    Xin Chaojun
    Xing Xiaochen
    [J]. PROCEEDINGS OF 2013 IEEE 11TH INTERNATIONAL CONFERENCE ON ELECTRONIC MEASUREMENT & INSTRUMENTS (ICEMI), 2013, : 631 - 635
  • [7] Trajectory optimization of advanced launch system
    Karsli, G
    Tekinalp, O
    [J]. RAST 2005: Proceedings of the 2nd International Conference on Recent Advances in Space Technologies, 2005, : 374 - 378
  • [8] Global positioning system detection of Minuteman II launch and positioning of launch site
    Hawarey, M
    Ayan, T
    [J]. JOURNAL OF SURVEYING ENGINEERING-ASCE, 2005, 131 (03): : 78 - 86
  • [9] ADVANCED MANNED LAUNCH SYSTEM COMPARISONS
    PILAND, WM
    TALAY, TA
    [J]. SPACE TECHNOLOGY-INDUSTRIAL AND COMMERCIAL APPLICATIONS, 1990, 10 (04): : 215 - 224
  • [10] Application Research of Big Data for Launch Support System at Space Launch Site
    Dong, Wei
    Xiao, Litian
    Niu, Shengfen
    Niu, Jianjun
    Wang, Fei
    [J]. PROCEEDINGS OF THE THIRD INTERNATIONAL CONFERENCE ON COMPUTER SCIENCE AND APPLICATION ENGINEERING (CSAE2019), 2019,