Control of launch vehicles as flexible bodies

机译：控制运载火箭作为灵活的机构

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A review of the control system designs of expendable launch vehicles is preseted terms of their flexibility, based on a seies of launching experimences in Japan. The equations of motion are formulated for both lateral and longitudinal dyhamics of the flexible vehicles. Aerodynamic loads casuded by wind during the atmospheric flight are described in conection with the trajectory planning. Mode analyses are carried out for launch vehicles, follwed by time responeses to the flight environment. Stability analyses for the lateral and longitudinal vibrations of launch vehicles are presented with a special empphsis on POGOs.

机译：根据日本的一系列发射经验，对消耗性运载火箭的控制系统设计进行了审查，以预先确定其灵活性。运动方程式针对柔性车辆的横向和纵向动力学而制定。在大气飞行过程中，由风引起的空气动力学载荷与轨迹规划相联系。根据对飞行环境的时间响应，对运载火箭进行模式分析。提出了运载火箭横向和纵向振动的稳定性分析，并带有关于POGO的特殊经验。

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来源
《4th IFAC(International Federation of Automatic Control) Symposium on Automatic Control in Aerospace 1998 Seoul, Korea, 24-28 August 1998》|1998年|p.323-334|共12页
会议地点 Seoul(KR)
作者
Hidehiko Mori;
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原文格式 PDF
正文语种 eng
中图分类航空、航天技术的研究与探索;
关键词
Attitude contrl; Mode analysis; oscillation; Stability analysis; space vehicles; Trajectory Planning; Vehicle dynamics.;

机译：态度控制；模式分析；振荡;稳定性分析；航天器；轨迹规划；车辆动力学。;

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专利

1. Control system design of flexible-body launch vehicles [J] . Hidehio Mori Control Engineering Practice . 1999,第9期

机译：柔性运载火箭的控制系统设计
2. Finite-time observer-based backstepping control of a flexible launch vehicle [J] . Duraffourg Elodie, Burlion Laurent, Ahmed-Ali Tarek Journal of vibration and control: JVC . 2018,第8期

机译：基于有限时间的柔性发动车辆的俯视性控制
3. Observer-based robust control for a flexible launch vehicle [J] . Ou Liuli, Liu Lei, Wang Yongji, Proceedings of the Institution of Mechanical Engineers . 2015,第I6期

机译：基于观察者的鲁棒控制，用于灵活的运载火箭
4. LQG Controller for Load Relief in theCombined Rigid Body and Flexibility Model of a Launch Vehicle [C] . Ammu Prameela Nandakumar, Lalu Seban, Rajesh Joseph Abraham, International Conference on Intelligent Computing, Instrumentation and Control Technologies . 2019

机译：LQG控制器用于运载火箭组合刚体和柔性模型中的载荷释放
5. Real Time Mode Sensing and Attitude Control of Flexible Launch Vehicle with Fiber Bragg Grating Sensor Array [D] . Jiang, Hao 2011

机译：光纤布拉格光栅传感器阵列的柔性运载火箭实时模式传感与姿态控制
6. Research on the Rapid and Accurate Positioning and Orientation Approach for Land Missile-Launching Vehicle [O] . Kui Li, Lei Wang, Yanhong Lv, 2015

机译：陆空导弹发射车快速准确的定位定向方法研究
7. 1SB-03 1SB-03 Body-cell dynamic mechano-mechanical linkage : softness, flexibility, fluctuation and controllability derived from ECM environment as "niche for cells in our body"(1SB Body-cell dynamic linkage: softness, flexibility, fluctuation and controllability,Symposium,The 50th Annual Meeting of the Biophysical Society of Japan) [O] . Yoriko Atomi, Miho Shimizu, Eri Fujita, 2012

机译：1SB-03 1SB-03体内细胞动态机械连接：柔软性，柔韧性，波动性和可控性，从ECM环境衍生为“我们身体细胞的Niche”（1SB体内细胞动态连杆：柔软性，柔韧性，波动和可控性，研讨会，日本生物物理学会的第50次年会）
8. A frequency independent technique for extracting the rigid-body motion from the total motion of a large flexible launch vehicle [R] . Howard, J. C. 1965

机译：一种独立于频率的技术，用于从大型柔性运载火箭的总运动中提取刚体运动

Control of launch vehicles as flexible bodies

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