作者： Xie, Wei¹;Wang, Hanping¹; （¹School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081, China）

出处： Guti Huojian Jishu/Journal of Solid Rocket Technology 2016 Vol.39 No.1 P146-149

摘要： Based on the interior ballistics theory and Craige-Bampton method, co-simulation platform of lift-draw vertical ejection system was established under ...

作者： Yang, Wu¹;Liu, Li¹;Zhou, Si-Da¹;Ma, Zhi-Sai¹; （¹Key Laboratory of Dynamics and Control of Flight Vehicle of Ministry of Education, Beijing Institute of Technology, Beijing, 100081, China）

出处： Jixie Gongcheng Xuebao/Journal of Mechanical Engineering 2016 Vol.52 No.3 P79-85

摘要： For modal parameter identification of time-varying structures, an improved identification approach is presented, which uses the moving least square me ...

作者： Hu, Chunsheng¹;Xu, Chengdong²;Fan, Guochao²;Song, Dan²; （¹School of Mechanical Engineering, Ningxia University, Yinchuan, 750021, Ningxia, China;²School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081, China）

出处： International Journal of Simulation: Systems, Science and Technology 2016 Vol.17 No.44 P33.1-33.6

摘要： Modularity is an effective way to handle complexity, and the design development process ismodularized in thecollaborative and integrated design proces ...

作者： 涂海峰，刘莉 （SCHOOl OF AEROSPACE ENGINEERING，BEIJING INSTITUTE OF TECHNOlOGy）

出处： 北京理工大学学报(英文版) 2016 第25卷 第1期 P28-34

关键词： compensation；compensated；recursive；estimator；quickly；drift；polynomial；removed；military；angular

摘要： In recent years,a large number of small volume,low cost micro electro mechanical systems(MEMS)digital three-axis angular rate gyroscopes have been dev ...

作者： 吴彦森，祁瑞 （School of Aerospace Engineering，Beijing Institute of Technology）

出处： Journal of Beijing Institute of Technology 2016 第A2期 P104-107

关键词： libration；point；orbit；nonlinear；periodic；system；characteristic；exponent；assignment；improved；state；feedback；control(ISFC)

摘要： An improved state feedback control(ISFC) scheme is proposed for station-keeping mission of satellite along unstable nonlinear period orbit near collin ...

作者： Yulong Yan，Baozeng Yue （School of Aerospace Engineering，Beijing Institute of Technology）

出处： 力学快报(英文版) 2016 第6卷 第2期 P100-106

关键词： Energy-Casimir；method；Liquid；sloshing；Nonlinear；stability；Flexible；appendage

摘要： The stability of partly liquid filled spacecraft with flexible attachment was investigated in this paper.Liquid sloshing dynamics was simplified as th ...

作者： CHEN Xin^1,2;LIU Li^1,2;ZHOU Sida^1,2;YUE Zhenjiang^1,2; （¹Key Laboratory of Dynamics and Control of Flight Vehicle of Ministry of Education,Beijing Institute of Technology;²School of Aerospace Engineering, Beijing Institute of Technology）

出处： Chinese Journal of Mechanical Engineering 2016 第29卷 第5期 P983-991

关键词： clustering；benchmark；capturing；fidelity；prior；adequately；adding；indispensable；squared；utilized

摘要： Reduced order models-ROMs) based on the snapshots on the CFD high-fidelity simulations have been paid great attention recently due to their capability ...

作者： SANGREGORIO Miguel，AHMADLOO Hamed，张景瑞，谢侃，王宁飞 （School of Aerospace Engineering，Beijing Institute of Technology）

出处： Journal of Beijing Institute of Technology 2016 第A2期 P15-20

关键词： space；debris；drag；sail；orbital；simulation；telescopic；technology；stretch；wrap

摘要： Regarding the current increment of LEO space debris and its negative effect on space missions in this environment,a new removal mechanism is proposed ...

作者： Chen Yongbo，Yu Jianqiao，Mei Yuesong，Zhang Siyu，Ai Xiaolin，Jia Zhenyue （School of Aerospace Engineering, Beijing Institute of Technology）

出处： 中国航空学报(英文版) 2016 第1期 P184-201

关键词： collaborative；assembling；trajectory；intelligent；constraint；faster；guarantee；freedom；sequential；coordinate

摘要： A hierarchic optimization strategy based on the offline path planning process and online trajectory planning process is presented to solve the traject ...

作者： Lei Juanmian，Zhao Shuai，Wang Suozhu （School of Aerospace Engineering, Beijing Institute of Technology）

出处： Chinese Journal of Aeronautics 2016 第4期 P914-923

关键词： aircraft；supersonic；vortex；turbulence；backward；averaged；utilized；Reynolds；positions；aerodynamic

摘要： This paper investigates the influence of forward-swept wing(FSW) positions on the aerodynamic characteristics of aircraft under supersonic condition(M ...