Compromise Optimal Design using Control-based Analysis of Hypersonic Vehicles

被引：3

作者：

Liu, Yanbin ^{[1
]}

Bing, Hua ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, Nanjing 210016, Jiangsu, Peoples R China

来源：

INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | 2015年 / 16卷 / 02期

基金：

中国国家自然科学基金;

关键词：

Hypersonic vehicles; Compromise optimal design; Dynamic characteristics; Flight stability; Parametric model; SLIDING MODE CONTROL; TRACKING CONTROL;

D O I：

10.5139/IJASS.2015.16.2.137

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Hypersonic vehicles exhibit distinct dynamic and static characteristics, such as unstable dynamics, strict altitude angle limitation, large control bandwidth, and unconventional system sensitivity. In this study, compromise relations between the dynamic features and static performances for hypersonic vehicles are investigated. A compromise optimal design for hypersonic vehicles is discussed. A parametric model for analyzing the dynamic and static characteristics is established, and then the optimal performance indices are provided according to the different design goals. A compromise optimization method to balance the dynamic and static characteristics is also discussed. The feasibility of this method for hypersonic vehicles is demonstrated.

引用

页码：137 / 147

页数：11

共 50 条

[21] Time optimal control-based RF pulse design under gradient imperfections
Aigner, Christoph S.
Rund, Armin
Seada, Samy Abo
Price, Anthony N.
Hajnal, Joseph, V
Malik, Shaihan J.
Kunisch, Karl
Stollberger, Rudolf
MAGNETIC RESONANCE IN MEDICINE, 2020, 83 (02) : 561 - 574
[22] Flight Envelope Prediction via Optimal Control-Based Reachability Analysis
Lu, Zhidong
Hong, Haichao
Gerdts, Matthias
Holzapfel, Florian
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2022, 45 (01) : 185 - 195
[23] Efficient object tracking using control-based observer design
Qu, Wei
Schonfeld, Dan
2006 IEEE INTERNATIONAL CONFERENCE ON MULTIMEDIA AND EXPO - ICME 2006, VOLS 1-5, PROCEEDINGS, 2006, : 1001 - +
[24] Dynamic surface control and active disturbance rejection control-based integrated guidance and control design and simulation for hypersonic reentry missile
Zhang, Cong
Wu, Yun-Jie
INTERNATIONAL JOURNAL OF MODELING SIMULATION AND SCIENTIFIC COMPUTING, 2016, 7 (03)
[25] Optimal Control-Based Strategy for Sensor Deployment
Ababnah, Ahmad
Natarajan, Balasubramaniam
IEEE TRANSACTIONS ON SYSTEMS MAN AND CYBERNETICS PART A-SYSTEMS AND HUMANS, 2011, 41 (01): : 97 - 104
[26] Safe Reinforcement Learning-Based Robust Approximate Optimal Control for Hypersonic Flight Vehicles
Shi, Lei
Wang, Xuesong
Cheng, Yuhu
IEEE TRANSACTIONS ON VEHICULAR TECHNOLOGY, 2023, 72 (09) : 11401 - 11414
[27] Nonlinear Disturbance Observer Based Fuel-consumption Optimal Control for Airbreathing Hypersonic Vehicles
Man, Chaoyuan
Bai, Jinfu
2020 IEEE 16TH INTERNATIONAL CONFERENCE ON CONTROL & AUTOMATION (ICCA), 2020, : 1535 - 1540
[28] Analysis of optimal initial glide conditions for hypersonic glide vehicles
Yan, X. (yan804@nwpu.edu.cn), 1600, Chinese Journal of Aeronautics (27):
[29] Feedback linearization-based robust nonlinear control design for hypersonic flight vehicles
Rehman, Obaid Ur
Petersen, Ian R.
Fidan, Baris
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2013, 227 (I1) : 3 - 11
[30] Analysis of optimal initial glide conditions for hypersonic glide vehicles
Yan Xiaodong
Lyu Shi
Tang Shuo
Chinese Journal of Aeronautics , 2014, (02) : 217 - 225

← 1 2 3 4 5 →