Non-stationary H infinity control law for launcher with bending modes

机译：具有弯曲模式的发射器的非平稳H无限控制律

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This paper presents the development of an H infinity robust control l aw for the atmospheric flight phase of a future Ariane's type launcher. Some particular points of the develoment are the launcher control problem transcription into H infinity methodology framework, the take into accoujnt of system non-stationary features and the problem of finding a simplified on-board implementation of H infinity law performances compared to an LQG control law reference and implemenatation solutions with an LQG type structure for H infinity controllers.

机译：本文介绍了用于未来阿丽亚娜型发射器的大气飞行阶段的H无限鲁棒控制系统的开发。开发的一些特殊点是将发射器控制问题转化为H无穷大方法框架，考虑到系统的非平稳特征以及与LQG控制定律相比找到简化的H无穷定律性能的机载实现的问题具有HQ无穷大控制器的LQG类型结构的参考和实现解决方案。

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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.433-438|共6页
会议地点 Seoul(KR)
作者
S.Mauffrey; M.Schoeeler;
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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
stability; performance, robustness; methology, H infiinity synthesis; implementation.;

机译：稳定性;性能，坚固性；方法学，H无限合成；实施。;

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专利

1. Predictive H/sub infinity / model reference optimal control law for SIMO systems [J] . Grimble M.J. IEE Proceedings. Part D . 1989,第6期

机译：SIMO系统的预测H /亚无穷大/模型参考最优控制律
2. Bending and Torsional Vibration Control of a Flexible Structure Using H-infinity Based Robust Control [J] . Toshiaki MIYAKURA, Kousei MIYAMOTO, Indra Narayan KAR 日本機械学会論文集. C編 . 1999,第635期

机译：基于H-∞的鲁棒控制的挠性结构的弯曲和扭转振动控制
3. Attitude controller design for reusable launch vehicles during reentry phase via compound adaptive fuzzy H-infinity control [J] . Qi Mao, Liqian Dou, Qun Zong, Aerospace science and technology . 2018,第JANa期

机译：复合自适应模糊H∞控制在再入阶段可重复使用运载火箭的姿态控制器设计。
4. Non-stationary H infinity control law for launcher with bending modes [C] . S.Mauffrey, M.Schoeeler International Federation of Automatic Control symposium on automatic control in aerospace . 1999

机译：具有弯曲模式的发射器非静止的H无限控制法
5. Development of a finite difference neighboring optimal control law and application to the optimal landing of a reusable launch vehicle. [D] . Wetzel, Todd Andrew. 1996

机译：有限差邻近最优控制律的发展及其在可重复使用运载火箭最优着陆中的应用。
6. Terminal Sliding Mode Control with a Novel Reaching Law and Sliding Mode Disturbance Observer for Inertial Stabilization Imaging Sensor [O] . Xin Che, Dapeng Tian, Ping Jia, 2020

机译：带有惯性稳定成像传感器的新型趋近律和滑模扰动观测器的终端滑模控制
7. Attitude controller design for reusable launch vehicles during reentry phase via compound adaptive fuzzy H-infinity control [O] . Qi Mao, Liqian Dou, Qun Zong, 2018

机译：态度控制器设计在重新使用的阶段在再入相位期间通过复合自适应模糊H-Infinity对照设计
8. Hypersonic vehicle model and control law development using H(infinity) and micron synthesis [R] . Gregory, Irene M., Chowdhry, Rajiv S., Mcminn, John D., 1994

机译：高超声速飞行器模型和控制法开发使用H（无限）和微米合成

Non-stationary H infinity control law for launcher with bending modes

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