作者： Abbas, Syed Zaheer¹;Nayak, Manoj Kumar²;Mabood, Fazle E.³;Dogonchi, Abdul Sattar⁴;Chu, Yuming^5,6;Khan, Waqar Azeem⁷;

摘要： Carbon nanotubes (CNTs) are characterized with exceptional electrical, thermal, mechanical, chemical, and optical properties (e.g., electrical conduct ...

作者： Tingting Zhang, Beijing Institute of Technology;Haoping SHE, Beijing Institute of Technology

出处： AIAA Atmospheric Flight Mechanics Conference

摘要： A guidance law with terminal impact angle constraint is presented, which can guide amissile in accordance with an elliptical trajectory to adapt its m ...

作者： Di Wu, Beijing Institute of Technology;Teng Long, Beijing Institute of Technology;Yan Wang, Beijing Institute of Technology;Li Liu, Beijing Institute of Technology

出处： 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference Dallas, TX

关键词： Aircraft Design;Airfoil;Optimization Algorithm;MATLAB;Internal Combustion Engines;Aeronautics;Computational Electromagnetics;Industrial Applications;Evolutionary Algorithm;Surrogate Model

摘要： Space-filling and projective properties of design of computer experiments (DoCE) methods are desired features for metamodeling. To pursue good perform ...

作者： Renhe Shi, Beijing Institute of Technology;Li Liu, Beijing Institute of Technology;Teng Long, Beijing Institute of Technology;Jian Liu, Beijing Institute of Technology

出处： 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

摘要： Radial basis function (RBF) surrogate model has been widely applied in engineeringdesign optimization problems. Ensemble of RBF (ERBF) combines indivi ...

作者： Zhengshi Yu, Beijing Institute of Technology;Zeduan Zhao, Beijing Institute of Technology;Pingyuan Cui, Beijing Institute of Technology

出处： AIAA Guidance, Navigation, and Control Conference

摘要： Atmospheric entry guidance is a necessary technology for a Mars pin-point landing in thefuture. For a preferred reference-tracking guidance, trajector ...

作者： Shaoming He, Beijing Institute of Technology;Defu Lin, Beijing Institute of Technology;Jiang Wang, Beijing Institute of Technology

出处： AIAA Guidance, Navigation, and Control Conference

摘要： In this paper, two composite inverse optimal guidance laws against maneuvering targets have been proposed and the stability analysis is also presented ...

作者： Shi Zhongjiao, Beijing Institute of Technology;Liangyu Zhao, Beijing Institute of Technology;Jiazhong Peng, Beijing Institute of Technology

出处： AIAA Atmospheric Flight Mechanics Conference

摘要： The coning motion is a basic angular behavior of spinning missiles. Research on thestability of coning motion is always active. In this paper, the int ...

作者： Tong Qin, Beijing Institute of Technology;Shengying Zhu, Beijing Institute of Technology;Pingyuan Cui, Beijing Institute of Technology

出处： AIAA Guidance, Navigation, and Control Conference

摘要： The Mars orbiter-lander integrated exploration has its attractiveness on better economyand more scientific return, for which the human’s first success ...

作者： Zhengshi Yu, Beijing Institute of Technology;Rui Xu, Beijing Institute of Technology;Pingyuan Cui, Beijing Institute of Technology

出处： AIAA Guidance, Navigation, and Control Conference

摘要： Pin-point landing is one of the key technologies for the future Mars landing explorations.However, the traditional navigation system in the powered de ...

作者： Yanting Xiong, Beijing Institute of Technology;Xin Sui, Beijing Institute of Technology;Ning-fei Wang, Beijing Institute of Technology

出处： 51st AIAA/SAE/ASEE Joint Propulsion Conference

摘要： NEPE propellant is a new kind of solid propellant developed in the 1980s containingblend nitrate ester plasticized polyether adhesive. By NEPE propell ...