AN ATTITUDE CONTROL SYSTEM FOR LARGE LAUNCH VEHICLES

被引：1
|
作者：
SELTZER, SM
机构：
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 1969年 / 6卷 / 06期
关键词：
D O I：
10.2514/3.29653
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：748 / +
页数：1
相关论文
共 50 条
  • [11] SAC-Based Intelligent Load Relief Attitude Control Method for Launch Vehicles
    Zhou, Shou
    Yang, Hao
    Zhang, Shifeng
    Bai, Xibin
    Wang, Feng
    AEROSPACE, 2025, 12 (03)
  • [12] Integrated architecture for navigation and attitude control of low-cost suborbital launch vehicles
    dos Santos, Pedro
    Oliveira, Paulo
    ACTA ASTRONAUTICA, 2024, 222 : 52 - 68
  • [13] An adaptive notch filtering approach with frequency holder for attitude control of flexible launch vehicles
    He, Xiao
    Yang, Jinzhao
    Liu, Yuxi
    Hu, Cunming
    Tan, Shujun
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2025, 97 (03): : 356 - 365
  • [14] A novel global sliding mode control strategy for attitude control of reusable launch vehicles in the reentry phase
    Wang, Liang
    Liu, Yunpeng
    Liu, Xiangdong
    PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 3615 - 3620
  • [15] Low cost guidance, navigation, and control system for launch vehicles
    Bauer, TP
    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM (STAIF-96), PTS 1-3: 1ST CONFERENCE ON COMMERCIAL DEVELOPMENT OF SPACE; 1ST CONFERENCE ON NEXT GENERATION LAUNCH SYSTEMS; 2ND SPACECRAFT THERMAL CONTROL SYMPOSIUM; 13TH SYMPOSIUM ON SPACE NUCLEAR POWER AND PROPULSION - FUTURE SPACE AND EARTH SCIENCE MISSIONS - SPECIAL TOPIC; REMOTE SENSING FOR COMMERCIAL, CIVIL AND SCIENCE APPLICATIONS - SPECIAL TOPIC, 1996, (361): : 617 - 622
  • [16] Control system design of flexible-body launch vehicles
    Mori, H
    CONTROL ENGINEERING PRACTICE, 1999, 7 (09) : 1163 - 1175
  • [17] LARGE LAUNCH VEHICLES - PRESENT AND FUTURE
    LUCAS, WR
    CRAWFORD, RG
    SAE TRANSACTIONS, 1969, 78 : 159 - &
  • [18] SMALL LAUNCH VEHICLES FOR LARGE TRAFFIC
    RUPPE, HO
    ASTRONAUTICS & AERONAUTICS, 1982, 20 (05): : 87 - 87
  • [19] OPTIMAL ATTITUDE CONTROL SYSTEM FOR SPINNING AEROSPACE VEHICLES
    SOHONI, VS
    GUILD, DR
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1970, 18 (02): : 86 - &
  • [20] Dynamic Integral Sliding Mode for Launch Vehicle Attitude Control System
    Wang, Zirui
    Liu, Lei
    Wang, Yongji
    Wang, Zhishen
    PROCEEDINGS OF THE 2012 24TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2012, : 1713 - 1718
12345