Fixed Order Robust Control Design for Hypersonic Vehicles
高超声速机的固定阶鲁棒控制器的设计
Hypersonic combined cycle engine concept with tandem layout
高超声速串联式组合动力装置方案
Dynamic Virtual Prototype Design of Hypersonic Cruise Vehicle
高超声速巡航飞行器动力学虚拟样机设计
Analyses of High Altitude Wind Model of Hypersonic Flight Test
高超声速飞行试验风场建模与仿真分析
Conceptual Design of an Airbreathing Hypersonic Civil Transport
吸气式高超声速民用运输机概念设计
Optimizing Research on Hypersonic Vehicle Skip Flying Trajectory
高超声速飞行器冲跃飞行轨迹优化研究
THE AERODYNAMICAL ANALYSIS OF BODY IN HYPERSONIC SOURCE FLOW FIELD
高超声速点泉流场中的气动力
Investigation of waverider configuration in hypersonic wind tunnel
乘波外形高超声速风洞测力试验研究
The forebody design a key issue for hypersonic airbreathing vehicle.
前体设计是吸气式高超声速飞行器设计的关键之一。
Exponential Approach Law Based Sliding Control for a Hypersonic Vehicle
基于指数趋近律的高超声速飞行器滑模控制器设计
A conceptual design of the hypersonic civil transport is introduced here.
介绍了高超声速民用运输机的概念设计方案。
The system will be capable of destroying hypersonic and ballistic targets.
该系统将能够摧毁超音速和弹道目标。
Adaptive Control Based on Characteristic Model for a Hypersonic Flight Vehicle
高超声速飞行器基于特征模型的自适应控制
Hypersonic pitching damp measurements for a winged vehicle by model free flight
有翼飞行器高超声速动导数的风洞自由飞测量
Numerical study of flow past hypersonic research vehicle with detaching booster
高超声速验证飞行器助推分离段流场数值研究
THE COMPUTATIONS OF ABLATIVE HYPERSONIC VISCOUS FLOWS IN CHEMICAL NONEQUILIBRIUM
有烧蚀气体产物影响的化学非平衡粘性流数值计算研究
Study on Blackout in Near Space Hypersonic Vehicle Radio Frequency Communication
近空间高超音速飞行器射频通信黑障研究
Flutter of Airfoil with Structural Nonlinearity in Supersonic and Hypersonic Flow
结构非线性机翼的超音速和高超音速颤振
Eigenvalue perturbation analysis of thrust law effects on hypersonic flight dynamics
高超声速飞行动态特性的特征值扰动分析
Several Problems of Flight Characteristics and Flight Control for Hypersonic Vehicles
高超声速飞行器飞行特性和控制的若干问题
In this thesis, the aerodynamic heating methods of hypersonic projectile are presented.
本论文进行了高超声速弹丸得气动热研究。
The computation and analysis for the hypersonic flow over reentry vehicles with ablation
高超声速再入体烧蚀流场计算分析
Aerodynamic and aerothermal numerical simulation of hypersonic lifting body configuration
高超声速升力体气动力气动热数值计算
Hypersonic aircraft refers to the speed of sound, at least 5 times more than the aircraft.
高超音速飞机是指超过音速至少5倍得飞机。
All these features make hypersonic flight control design a great challenge to researchers.
这些特点使得高超声速飞行器的飞行控制设计极具挑战性。
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