Flight Dynamics 2009 Issue 5 Qualities Assesses Criterion of Short Period Mode for Flying Wings with Low Aspect-Ratio

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Flight Dynamics
1002-0853
2009 Issue 5

Qualities Assesses Criterion of Short Period Mode for Flying Wings with Low Aspect-Ratio

..............page:21-24

Survey of Cooperative Path Planning for Multiple UAVs

..............page:1-5,10

Development and Technologies to the Study of Civil Aircraft Icing

..............page:11-14

fei xing li xue zheng gao jian ze

..............page:封底

Key Technologies in Morphing Aircraft Design

..............page:6-10

Design and Validity Check of a Wing-Boathouse Aero Craft

..............page:79-81,93

Modeling Area Air Traffic Flow Control

..............page:86-88,93

Designing and Optimizing the Berthing Orbit of the Anti-Orbit Interceptor

..............page:63-65

Design Method of Guidance Handing-Over Bound Based on System with Stochastic Jump Structures

..............page:55-58,74

Trimming for Aircraft with Multiple Control Effectors Based on Flight Performance Optimization

..............page:17-20

Analysis and Design of Maneuvering Load Control System During Aircraft Level Flight

..............page:25-28

Virtual-Leader Based Impact Time and Impact Angle Control

..............page:51-54

Angular Motion Models for Ultra Range Rocket in High Altitude Environment

..............page:66-69

Effect of Solar Radiation Pressure on the ER3BP Lagrange Points

..............page:70-74

Air Traffic Flow Control Based on Eulerian Model

..............page:94-96

Line-of-Sight (LOS) Dynamic Equation in Spherical Gravitational Field

..............page:82-85

Flight Orbit Design of Rover to the Mars

..............page:40-43

Hardware-in-the-Loop Flight Simulate Experimental Platform Designed for UAVs

..............page:75-78

Study on Path Planning with Sudden Appearing Threats

..............page:89-93

Optimization of Aircraft Flight Control System Based on Evolutionary Strategy

..............page:33-36

Geometry Representation Method of Airfoil Based on Free Form Deformation

..............page:44-46,50

Forecast Variable Structure Midcourse Guidance Law Design for Supersonic Intercept Missile

..............page:47-50

Yaw Control of a Flying-Wing Aircraft Based on Nonlinear Control Allocation

..............page:29-32

Terminal Area Energy Management of Suborbital Vehicle Based on Range Control

..............page:59-62

Application of Digital Technology to the Designing and Manufacturing for a Fighter

..............page:15-16,28

Study of the Wing Shape of Flapping-Wing MAV

..............page:37-39,43