Get 20M+ Full-Text Papers For Less Than $1.50/day. Start a 14-Day Trial for You or Your Team.

Learn More →

Overview of control-centric integrated design for hypersonic vehicles

Overview of control-centric integrated design for hypersonic vehicles Abstract Hypersonic vehicles (HSVs) exhibit significant advantages over other vehicles, including the wide range of velocity and large airspace types, and these features have contributed to the rapid development of HSVs in the last 20 years. Moreover, hypersonic technologies have become a multidisciplinary research topic in the fields of aerodynamics, propulsion, structure, material, and control. Different types of re-entry gliding, air-breathing cruise, and aerospace vehicles have been designed to realize ambitious tasks, which in turn influenced the technological advancements and process change in the military. This paper summarizes the control-oriented integrated design of HSVs. First, the status of current research on the distinct characteristics and technique issues of HSVs is introduced. Then, the progresses made on complex modeling, guidance and control, and trajectory optimization are elaborated to exhibit the significant research interest in hypersonic technologies. The control-integrated design of HSVs is emphasized to solve the multidisciplinary design problems associated with the model and its control and trajectory. Various strategies regarding the multidisciplinary optimization design are also proposed to solve the integrated design problem. Finally, suggestions are provided for the control-oriented integrated design of HSVs. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Astrodynamics Springer Journals

Overview of control-centric integrated design for hypersonic vehicles

Liu, Yanbin; Chen, Boyi; Li, Yuhui; Shen, Haidong
Astrodynamics , Volume 2 (4): 18 – Dec 1, 2018
Download PDF
18 pages

Loading next page...
 
/lp/springer-journals/overview-of-control-centric-integrated-design-for-hypersonic-vehicles-O6Q4mQEdsl
Publisher
Springer Journals
Copyright
2018 Tsinghua University Press
ISSN
2522-008X
eISSN
2522-0098
DOI
10.1007/s42064-018-0027-8
Publisher site
See Article on Publisher Site

Abstract

Abstract Hypersonic vehicles (HSVs) exhibit significant advantages over other vehicles, including the wide range of velocity and large airspace types, and these features have contributed to the rapid development of HSVs in the last 20 years. Moreover, hypersonic technologies have become a multidisciplinary research topic in the fields of aerodynamics, propulsion, structure, material, and control. Different types of re-entry gliding, air-breathing cruise, and aerospace vehicles have been designed to realize ambitious tasks, which in turn influenced the technological advancements and process change in the military. This paper summarizes the control-oriented integrated design of HSVs. First, the status of current research on the distinct characteristics and technique issues of HSVs is introduced. Then, the progresses made on complex modeling, guidance and control, and trajectory optimization are elaborated to exhibit the significant research interest in hypersonic technologies. The control-integrated design of HSVs is emphasized to solve the multidisciplinary design problems associated with the model and its control and trajectory. Various strategies regarding the multidisciplinary optimization design are also proposed to solve the integrated design problem. Finally, suggestions are provided for the control-oriented integrated design of HSVs.

Journal

Astrodynamics – Springer Journals

Published: Dec 1, 2018

References

  • Some control problems for near space hypersonic vehicles
    C. Y. Sun, C. X. Mu, Y. Yu
  • Control relevant design optimization for air-breathing hypersonic vehicle considering performance limitation
    Y. P. Lu, B. Y. Chen, Y. B. Liu, D. B. Xiao
  • The stability analysis of rolling motion of hypersonic vehicles and its validations
    Y. D. Ye, Z. L. Zhao, H. Tian, X. F. Zhang
  • An overview of selected NASP aeroelastic studies at the NASA Langley Research Center
    M. D. Gibbons
  • Analysis of the development status and the defense problem of near space hypersonic vehicle
    X. G. Liang, H. L. Tian
  • A flexible hypersonic vehicle model developed with piston theory
    M. A. Bolender
  • Aeroelastic and aerothermoelastic analysis in hypersonic flow: past, present, and future
    J. J. Mcnamara, P. P. Friedmann
  • An overview on flight dynamics and control approaches for hypersonic vehicles
    B. Xu, Z. K. Shi
  • Hypersonic vehicle flight dynamics with coupled aerodynamic and reduced-order propulsive models
    J. F. Driscoll
  • Hypersonic vehicle simulation model: winged-cone configuration
    C. I. Cruz
  • Analytical aeropropulsive/aeroelastic hypersonic-vehicle model with dynamic analysis
    F. R. Chavez, D. K. Schmidt
  • Control-oriented modeling of an air-breathing hypersonic vehicle
    J. T. Parker, A. Serrani, S. Yurkovich, M. A. Bolender, D. B. Doman
  • A review on simulation-based optimization methods applied to building performance analysis
    A. T. Nguyen, S. Reiter, P. Rigo
  • Multifidelity surrogate modeling of experimental and computational aerodynamic data sets
    Y. Kuya, K. Takeda, X. Zhang, A. I. J. Forrester
  • Adaptive multifidelity constraints method for effcient multidisciplinary missile design framework
    N. V. Nguyen, M. Tyan, S. Jin
  • Sensitivity analysis of performance for control-oriented model of an air-breathing hypersonic vehicle
    Y. B. Liu
  • Sensitivity of flight dynamics of hypersonic vehicles to design parameters
    S. M. Torrez
  • Finding important independent variables through screening designs: a comparison of methods
    L. Trocine
  • Key criteria and selection of sensitivity analysis methods applied to natural resource models
    L. Ma
  • A review on global sensitivity analysis methods
    B. Iooss
  • Recent advances in surrogate-based optimization
    A. I. J. Forrester, A. J. Keane
  • Aspects of the matlab toolbox DACE
    H. B. Nielsen
  • Longitudinal long-term modes in super- and hypersonic flight
    G. Sachs
  • Path-attitude decoupling and flying qualities implications in hypersonic flight
    G. Sachs
  • Performance limitation of tracking control problem for a class of references
    H. Okajima, T. Asai
  • Performance limitations of nonminimum phase affne nonlinear systems
    H. N. Foghahaayee, M. B. Menhaj, H. A. Talebi, M. Khoshnam
  • Nonlinear adaptive control design for non-minimum phase hypersonic vehicle models with minimal control authority
    L. Fiorentini
  • Nonlinear control of non-minimum phase hypersonic vehicle models
    M. A. Bolender
  • Fundamental limitations in filtering and control
    J. H. Braslavsky
  • Multivariate feedback control
    S. Skogestad, I. Postlethwaite
  • An explicit description of null controllable regions of linear systems with saturating actuators
    T. S. Hu, Z. L. Lin, L. Qiu
  • Stability region for a class of open-loop unstable linear systems: theory and application
    L. Scibile, B. Kouvaritakis
  • The role of guidance, navigation, and control in hypersonic vehicle multidisciplinary design and optimization
    D. D. Moerder
  • Fundamental limitation on achievable decentralized performance
    V. Kariwala
  • Feedback limitations in nonlinear systems: from Bode integrals to cheap control
    M. M. Seron, J. H. Braslavsky, P. V. Kokotovic, D. Q. Mayne
  • Input performance limitations of feedback control
    J. F. Forbes
  • Survey of numerical methods for trajectory optimization
    J. T. Betts
  • A survey of trajectory optimization and guidance for hypersonic gliding vehicle
    C. Q. Huang, H. F. Guo, D. L. Ding
  • Generic framework for multi-disciplinary trajectory optimization of aircraft and power plant integrated systems
    R. Navaratne, M. Tessaro, W. Q. Gu, V. Sethi, P. Pilidis, R. Sabatini, D. Zammit-Mangion
  • A sparse nonlinear optimization algorithm
    J. T. Betts, P. D. Frank
  • Trajectory optimization using multiresolution techniques
    S. Jain, P. Tsiotras
  • A multiresolution technique-based gliding vehicle trajectory optimization algorithm
    X. Q. Chen, Z. X. Hou, J. X. Liu
  • Nonlinear estimation of hypersonic state trajectories in Bayesian framework with polynomial chaos
    P. Dutta, R. Bhattacharya
  • Trajectory optimization for hypersonic gliding vehicle considering stochastic disturbance
    H. F. Guo, C. Q. Huang, D. L. Ding, H. Xiao
  • Flight dynamics and feedback guidance issues for hypersonic airbreathing vehicles
    D. K. Schmidt
  • Shuttle entry guidance
    J. C. Harpold
  • Gliding guidance of high L/D hypersonic vehicles
    S. Forbes
  • Real-time optimal trajectory generation for constrained dynamical systems
    M. B. Milam
  • Optimal nonlinear guidance with inner-loop feedback for hypersonic re-entry
    D. G. MacMynowski
  • Gregory, I. M., Chowdhry, R. S., Mcminn, J. D., Shaughnessy, J. D. Hypersonic vehicle model and control law development using H and synthesis. NASA Technical Memorandum 4562, National Aeronautics and Space Administration, 1994.
    Gregory, I. M., Chowdhry, R. S., Mcminn, J. D., Shaughnessy, J. D. Hypersonic vehicle model and control law development using H and synthesis. NASA Technical Memorandum
  • Robust linear output feedback control of an airbreathing hypersonic vehicle
    D. O. Sigthorsson, P. Jankovsky, A. Serrani, S. Yurkovich, M. A. Bolender, D. B. Doman
  • Reference command tracking for a linearized model of an air-breathing hypersonic vehicle
    M. A. Bolender
  • Adaptive control of hypersonic vehicles in the presence of thrust and actuator uncertainties
    T. E. Gibson
  • Altitude and velocity tracking control for an airbreathing hypersonic cruise vehicle
    P. Ioannou
  • Development of linear- parameter-varying models for aircraft
    A. Marcos, G. J. Balas
  • Development of linear parameter-varying models of hypersonic air-breathing vehicles
    D. O. Sigthorsson
  • PV control design for over-actuated hypersonic vehicles models
    M. A. Bolender
  • Multi-loop gain- scheduling control of flexible air-breathing hypersonic vehicle
    D. M. Ge, X. L. Huang, H. J. Gao
  • Polytopic LPV modeling and gain-scheduled switching control for a flexible air-breathing hypersonic vehicle
    Y. Q. Huang, C. Y. Sun, C. S. Qian, J. M. Zhang, L. Wang
  • Switching LPV control designs using multiple parameter-dependent Lyapunov functions
    B. Lu, F. Wu
  • Switching LPV control method in wide flight envelope for hypersonic vehicles
    Z. H. Zhang, L. Y. Yang, G. Z. Shen
  • Control design for a hypersonic aircraft using a switched linear parameter-varying system approach
    Q. G. Lu, L. X. Zhang, P. Shi, H. R. Karimi
  • Switching control of a hypersonic vehicle based on guardian maps
    D. B. Xiao, M. Y. Liu, Y. B. Liu, Y. P. Lu
  • Gain scheduling with guardian maps for longitudinal flight control
    D. Saussié, L. Saydy, O. Akhrif, C. Bérard
  • Robust parameter dependent receding horizon H∞ control of flexible air-breathing hypersonic vehicles with input constraints
    W. W. Qin, J. Y. Liu, G. Liu, B. He, L. X. Wang
  • Feedback linearization and guaranteed cost control of uncertain nonlinear systems and its application to an air-breathing hypersonic flight vehicle
    O. U. Rehman
  • Reference command tracking control for an air-breathing hypersonic vehicle with parametric uncertainties
    G. Gao, J. Z. Wang
  • Robust minimax optimal control of nonlinear uncertain systems using feedback linearization with application to hypersonic flight vehicles
    B. Fidan
  • Evaluation of longitudinal desired dynamics for dynamic-inversion controlled generic reentry vehicles
    J. Georgie, J. Valasek
  • Reentry flight controller design using nonlinear dynamic inversion
    R. R. Costa, Q. P. Chu, J. A. Mulder
  • Robust flight control using incremental nonlinear dynamic inversion and angular acceleration prediction
    S. Sieberling, Q. P. Chu, J. A. Mulder
  • Nonlinear control of an airbreathing hypersonic vehicle: a backstepping approach
    H. Piet-Lahanier
  • Output feedback back-stepping control for a generic hypersonic vehicle via small-gain theorem
    Q. Zong, Y. H. Ji, F. L. Zeng, H. L. Liu
  • Adaptive backstepping control for air-breathing hypersonic vehicle with actuator dynamics
    Q. L. Hu, Y. Meng
  • Nonlinear disturbance observer based robust backstepping control for a flexible air-breathing hypersonic vehicle
    G. H. Wu, X. Y. Meng
  • Guaranteeing preselected tracking quality for air-breathing hypersonic non-affne models with an unknown control direction via concise neural control
    X. W. Bu, D. Z. Wei, X. Y. Wu, J. Q. Huang
  • Adaptive fuzzy back-stepping control of a flexible air-breathing hypersonic vehicle subject to input constraints
    P. F. Wang, J. Wang, X. W. Bu, C. Luo, S. L. Tan
  • New methodologies for adaptive sliding mode control
    F. Plestan, Y. Shtessel, V. Brgeault, A. Poznyak
  • Homogeneity approach to high-order sliding mode design
    A. Levant
  • Dynamic sliding mode control design
    A. J. Koshkouei, K. J. Burnham, A. S. I. Zinober
  • Adaptive high-order dynamic sliding mode control for a flexible air-breathing hypersonic vehicle
    Q. Zong, J. Wang, Y. Tao
  • Flight control for a flexible air-breathing hypersonic vehicle based on quasi-continuous high-order sliding mode
    J. Wang, Q. Zong, B. L. Tian, H. L. Liu
  • Continuous high order sliding mode controller design for a flexible air- breathing hypersonic vehicle
    J. Wang, Q. Zong, R. Su, B. L. Tian
  • Quasi-continuous high-order sliding mode controller and observer design for flexible hypersonic vehicle
    Q. Zong, J. Wang, B. L. Tian, Y. Tao
  • Unstable, nonminimum phase, nonlinear tracking by trajectory linearization control
    R. Huang
  • Sliding mode based trajectory linearization control for hypersonic reentry vehicle via extended disturbance observer
    X. L. Shao, H. L. Wang
  • Active disturbance rejection based trajectory linearization control for hypersonic reentry vehicle with bounded uncertainties
    X. L. Shao, H. L. Wang
  • Uncertainty analysis and robust trajectory linearization control of a flexible air-breathing hypersonic vehicle
    Z. Q. Pu, X. M. Tan, G. L. Fan, J. Q. Yi
  • Tracking performance and global stability guaranteed neural control of uncertain hypersonic flight vehicle
    T. Teng, C. G. Yang, S. L. Dai, M. Wang
  • Robust model predictive tracking control of hypersonic vehicles in the presence of actuator constraints and input delays
    W. W. Qin, B. He, G. Liu, P. T. Zhao
  • Disturbance observer-based L1 robust tracking control for hypersonic vehicles with T-S disturbance modeling
    Y. Yi, L. B. Xu, H. Shen, X. X. Fan
  • Disturbance observer-based antiwindup control for air-breathing hypersonic vehicles
    H. An, J. X. Liu, C. H. Wang, L. Wu
  • Approximate feedback linearization of an air-breathing hypersonic vehicle
    M. A. Bolender
  • An integrated optimization of hypersonic forebody/inlet based on surrogate models
    X. Y. Wu, R. Liu, S. B. Luo, Z. G. Wang
  • Multidisciplinary optimization of airbreathing hypersonic vehicles
    K. G. Bowcutt
  • Uncertainty propagation in hypersonic aerothermoelastic analysis
    N. Lamorte, B. Glaz, P. P. Friedmann, A. J. Culler, A. R. Crowell, J. A. McNamara
  • Aeroservoelastic modeling and analysis of a six-DOF hypersonic flight vehicle
    Q. Zong, M. You, F. L. Zeng, L. Q. Dou
  • Application of the 3D multi-block CST method to hypersonic aircraft optimization
    C. Z. Liu, Y. H. Duan, J. S. Cai, J. F. Wang
  • Dynamic stability analysis of hypersonic transport during reentry
    G. P. Guruswamy
  • Pigeon-inspired optimization applied to constrained gliding trajectories
    J. Zhao, R. Zhou
  • Automatic load relief numerical predictor-corrector guidance for low L/D vehicles return from low Earth orbit
    B. Zhang, S. Tang, B. F. Pan
  • Optimal control problems with stopping constraints
    Q. Lin, R. Loxton, K. L. Teo, Y. H. Wu