A SHORT HISTORY OF THE SPACE SHUTTLE ORBIT FLIGHT CONTROL SYSTEM DEVELOPMENT AND APPLICATION EVOLUTION

被引:0
|
作者
Hattis, Philip D. [1 ]
机构
[1] Charles Stark Draper Lab Inc, Complex Solut Div, 555 Technol Sq, Cambridge, MA 02139 USA
来源
关键词
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The Space Shuttle Orbit Flight Control System (OFCS) provided all Guidance, Navigation, and Control capabilities from external tank separation during ascent until entry interface during return. Its development began in earnest in 1975 with first orbital flight application in 1981. The many operational requirements for the Shuttle and its unique vehicle design characteristics demanded specialized algorithms and numerous functional features despite very limited computer memory and speed by contemporary standards. This paper provides a short history of the Shuttle OFCS development and orbital application evolution.
引用
收藏
页码:573 / 588
页数:16
相关论文
共 50 条
  • [31] Application of Optimal Control Techniques to the Parafoil Flight of Space Rider
    Michele Lucrezia
    Aerotecnica Missili & Spazio, 2024, 103 (2): : 117 - 128
  • [32] Development of a Flight Control System for an Ultralight Airplane
    Srovnal, Vilem, Jr.
    Kotzian, Jiri
    2008 INTERNATIONAL MULTICONFERENCE ON COMPUTER SCIENCE AND INFORMATION TECHNOLOGY (IMCSIT), VOLS 1 AND 2, 2008, : 692 - 697
  • [33] Immune System Dysregulation Occurs During Short Duration Spaceflight On Board the Space Shuttle
    Brian Crucian
    Raymond Stowe
    Satish Mehta
    Peter Uchakin
    Heather Quiriarte
    Duane Pierson
    Clarence Sams
    Journal of Clinical Immunology, 2013, 33 : 456 - 465
  • [34] Immune System Dysregulation Occurs During Short Duration Spaceflight On Board the Space Shuttle
    Crucian, Brian
    Stowe, Raymond
    Mehta, Satish
    Uchakin, Peter
    Quiriarte, Heather
    Pierson, Duane
    Sams, Clarence
    JOURNAL OF CLINICAL IMMUNOLOGY, 2013, 33 (02) : 456 - 465
  • [35] A political history of NASA's space shuttle: the development years, 1972-1982
    Woods, Brian
    SOCIOLOGICAL REVIEW, 2009, 57 : 25 - 46
  • [36] COMPUTER SIMULATION OF SPACE SHUTTLE ORBITER ENVIRONMENTAL THERMAL CONTROL-SYSTEM
    BARKER, RS
    JASIN, JJ
    MECHANICAL ENGINEERING, 1972, 94 (10) : 61 - &
  • [37] DEVELOPMENT OF THE PERSONAL PARACHUTE ASSEMBLY FOR THE SPACE-SHUTTLE CREW ESCAPE SYSTEM
    HERR, MD
    AIAA 10TH AERODYNAMIC DECELERATOR SYSTEMS TECHNOLOGY CONFERENCE: A COLLECTION OF TECHNICAL PAPERS, 1989, : 193 - 201
  • [38] Application of eigenstructure assignment to the design of flight control system
    Wu, Wen-Hai
    Shen, Chun-Lin
    Liu, Guo-Gang
    Geng, Chang-Mao
    Wang, Yu-Rong
    Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2002, 34 (05): : 639 - 642
  • [39] Development and application of an integrated framework for small UAV flight control development
    Paw, Yew Chai
    Balas, Gary J.
    MECHATRONICS, 2011, 21 (05) : 789 - 802
  • [40] 7.5.3 If I Could Do That, Then I Could… System Engineering in a Research and Development Environment - As Illustrated by the Evolution of the Space Shuttle Tiles
    Forsberg, Kevin
    INCOSE International Symposium, 1995, 5 (01): : 998 - 1012