Optimal Periodic Control of Hypersonic Cruise Vehicle
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- 英文论文题名：Optimal Periodic Control of Hypersonic Cruise Vehicle
- 论文作者：Wang Wenkai ; Hou Zhongxi ; Shan Shangqiu ; Guo Tianhao ; Chen Lili
- 英文论文作者：Wang Wenkai ; Hou Zhongxi ; Shan Shangqiu ; Guo Tianhao ; Chen Lili ; College of Aerospace Science and Technology ; National University of Defense Technology
- 年：2017
- 作者机构：College of Aerospace Science and Technology,National University of Defense Technology;
- 英文论文关键词：Hypersonic cruise vehicle ; Fuel efficiency ; Heat accumulation ; Optimal periodic cruise trajectory
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（B）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（B）
- 语种：英文
- 分类号：V448
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：6
- 文件大小：407k
- 原文格式：D
- 会议级别：全国
摘要
Object of this work is hypersonic cruise vehicle which cruises at Mach number beyond 5 in atmosphere. Range of this vehicle is often restricted by the poor aerodynamic, propulsive and structural performances and severe persistent aerodynamic heating. To extend its range, optimal periodic cruise trajectory has been adopted herein to improve fuel efficiency and remit heat accumulation. The performance measure is a weighted combination of the two factors. The simulations show that the two factors are mutually contradicted with variation of weighting factor, and that improvement of aerodynamic heating is much more distinct than that of fuel efficiency. The study on single period is helpful to design the whole flight envelop in future research.
Object of this work is hypersonic cruise vehicle which cruises at Mach number beyond 5 in atmosphere. Range of this vehicle is often restricted by the poor aerodynamic, propulsive and structural performances and severe persistent aerodynamic heating. To extend its range, optimal periodic cruise trajectory has been adopted herein to improve fuel efficiency and remit heat accumulation. The performance measure is a weighted combination of the two factors. The simulations show that the two factors are mutually contradicted with variation of weighting factor, and that improvement of aerodynamic heating is much more distinct than that of fuel efficiency. The study on single period is helpful to design the whole flight envelop in future research.
Object of this work is hypersonic cruise vehicle which cruises at Mach number beyond 5 in atmosphere. Range of this vehicle is often restricted by the poor aerodynamic, propulsive and structural performances and severe persistent aerodynamic heating. To extend its range, optimal periodic cruise trajectory has been adopted herein to improve fuel efficiency and remit heat accumulation. The performance measure is a weighted combination of the two factors. The simulations show that the two factors are mutually contradicted with variation of weighting factor, and that improvement of aerodynamic heating is much more distinct than that of fuel efficiency. The study on single period is helpful to design the whole flight envelop in future research.
引文
[1]J.Steelant,R.Varvill,and S.Defoort et al.,Achievement Obtained for sustained Hypersonic Flight within the LAPCAT-II Project,in 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference,Glasgow,AIAA-2015-3677,2015.
[2]J.Speyer,D.Dannemiller and D.Walker,Periodic Optimal Cruise of a Hypersonic Vehicle,in Guidance,Navigation,and Control and Co-located Conferences,338–346,AIAA-80-1777,1980.
[3]C.Chuang and H.Morimoto,Optimal Periodic Cruise for a Hypersonic Vehicle with Constraints,in Guidance,Navigation,and Control and Co-located Conferences,AIAA-96-3876,1996.
[4]B.Kang,D.Spencer and S Tang et al.,Optimal Periodic Cruise Trajectory via a Two-Level Optimization Method,Journal of Spacecraft and Rockets,47(4):597–613,2010.
[5]R.Li and Y.Shi,The Fuel Optimal Control Problem of a Hypersonic Aircraft with Periodic Cruising Mode,Mathematical and Computer Modelling,55(2012):2141–2150,2012.
[6]D.Chai,Y.Fang and Y.Wu et al.,Boost-skipping Trajectory Optimization for Air-breathing Hypersonic Missile,Aerospace Science and Technology,46(2015):506–513,2015.
[7]W.Haitao,Z.Dongbin and S.Mingwei,Optimization of Periodic Optimal Cruise for a Hypersonic Vehicle,in Chinese Automation Congress(CAC),2013,IEEE,2013:571–576.
[8]I.Houchin,The Rise and Fall of Dyna-Soar:a History of Air Force Hypersonic R&D,1944-1963,AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH,1995.
[9]M.Ferraiuolo and O.Manca,Heat Transfer in a Multilayered Thermal Protection System Under Aerodynamic Heating,International Journal of Thermal Sciences,53(2012):56–70,2012.
[10]J.Anderson,Introduction to Flight(Seventh Edition).Boston:Mc Graw-Hill,2005,chapter 10.
[11]H.Morimoto and J.Chuang,Minimum-fuel Trajectory along Entire Flight Profile for a Hypersonic Vehicle with Constraint,in AIAA Guidance,Navigation,and Control Conference and Exhibit,212–224,1998.
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[14]A.Wchter and T.Biegler,On the implementation of a primal-dual interior point filter line search algorithm for large-scale nonlinear programming,Mathematical Programming,106:25–57,2006.
[15]D.Kirk,Optimal Control Theory:An Introduction.New York:Dover Publications,Inc.,2004.
[16]R.Evans,Optimal Periodic Control Theory.Tech.rep.,U.S.Air Force Systems Command,1980.
[17]D.Grass,J.Caulkins,and G.Feichtinger et al.,Optimal Control of Nonlinear Processes:With Applications in Drugs,Corruption,and Terror,Berlin:Springer-Verlag,2008.
[2]J.Speyer,D.Dannemiller and D.Walker,Periodic Optimal Cruise of a Hypersonic Vehicle,in Guidance,Navigation,and Control and Co-located Conferences,338–346,AIAA-80-1777,1980.
[3]C.Chuang and H.Morimoto,Optimal Periodic Cruise for a Hypersonic Vehicle with Constraints,in Guidance,Navigation,and Control and Co-located Conferences,AIAA-96-3876,1996.
[4]B.Kang,D.Spencer and S Tang et al.,Optimal Periodic Cruise Trajectory via a Two-Level Optimization Method,Journal of Spacecraft and Rockets,47(4):597–613,2010.
[5]R.Li and Y.Shi,The Fuel Optimal Control Problem of a Hypersonic Aircraft with Periodic Cruising Mode,Mathematical and Computer Modelling,55(2012):2141–2150,2012.
[6]D.Chai,Y.Fang and Y.Wu et al.,Boost-skipping Trajectory Optimization for Air-breathing Hypersonic Missile,Aerospace Science and Technology,46(2015):506–513,2015.
[7]W.Haitao,Z.Dongbin and S.Mingwei,Optimization of Periodic Optimal Cruise for a Hypersonic Vehicle,in Chinese Automation Congress(CAC),2013,IEEE,2013:571–576.
[8]I.Houchin,The Rise and Fall of Dyna-Soar:a History of Air Force Hypersonic R&D,1944-1963,AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH,1995.
[9]M.Ferraiuolo and O.Manca,Heat Transfer in a Multilayered Thermal Protection System Under Aerodynamic Heating,International Journal of Thermal Sciences,53(2012):56–70,2012.
[10]J.Anderson,Introduction to Flight(Seventh Edition).Boston:Mc Graw-Hill,2005,chapter 10.
[11]H.Morimoto and J.Chuang,Minimum-fuel Trajectory along Entire Flight Profile for a Hypersonic Vehicle with Constraint,in AIAA Guidance,Navigation,and Control Conference and Exhibit,212–224,1998.
[12]F.Bonnans,P.Martinon and D.Giogi,et al.,BOCOP2.0.4-User Guide,http://bocop.org,November 2015.
[13]A.Walther and A.Griewank,Getting started with adol-c,in Combinatorial Scientific Computing,U.Naumann and O.Schenk.Chapman-Hall CRC Computational Science,2012.
[14]A.Wchter and T.Biegler,On the implementation of a primal-dual interior point filter line search algorithm for large-scale nonlinear programming,Mathematical Programming,106:25–57,2006.
[15]D.Kirk,Optimal Control Theory:An Introduction.New York:Dover Publications,Inc.,2004.
[16]R.Evans,Optimal Periodic Control Theory.Tech.rep.,U.S.Air Force Systems Command,1980.
[17]D.Grass,J.Caulkins,and G.Feichtinger et al.,Optimal Control of Nonlinear Processes:With Applications in Drugs,Corruption,and Terror,Berlin:Springer-Verlag,2008.