| no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
| 1 |
Aerodynamic pitch control design for reversal of missile’s flight direction
|
Kim, Yoonsoo
|
|
2014
|
228 |
9 |
p. 1519-1527
|
article
|
| 2 |
Approximate analytical solutions of an axially moving spacecraft appendage subjected to tip mass
|
Ghaleh, P Bagheri
|
|
2014
|
228 |
9 |
p. 1487-1497
|
article
|
| 3 |
A preliminary method to estimate impacts of inlet flow distortion on boundary layer ingesting propulsion system design point performance
|
Liu, Chengyuan
|
|
2014
|
228 |
9 |
p. 1528-1539
|
article
|
| 4 |
Command filtered back-stepping control of a flexible air-breathing hypersonic flight vehicle
|
Ji, Yuehui
|
|
2014
|
228 |
9 |
p. 1617-1626
|
article
|
| 5 |
Design optimization of aerodynamic shapes of a wing and its winglet using modified quantum-behaved particle swarm optimization algorithm
|
Wei, Zhang
|
|
2014
|
228 |
9 |
p. 1638-1647
|
article
|
| 6 |
Fault tree analysis for composite structural damages
|
Chen, Xi
|
|
2014
|
228 |
9 |
p. 1466-1474
|
article
|
| 7 |
Flight testing of noise abating required navigation performance procedures and steep approaches
|
Toebben, Helmut H
|
|
2014
|
228 |
9 |
p. 1586-1597
|
article
|
| 8 |
Huber-based divided difference filter with application to relative navigation
|
Li, Wei
|
|
2014
|
228 |
9 |
p. 1475-1486
|
article
|
| 9 |
Non-linear idealisation error analysis of an aerospace stiffened panel loaded in compression
|
Hetey, Laszlo
|
|
2014
|
228 |
9 |
p. 1574-1585
|
article
|
| 10 |
Numerical analysis of a swept wing hot air ice protection system
|
Bu, Xueqin
|
|
2014
|
228 |
9 |
p. 1507-1518
|
article
|
| 11 |
Optimal preliminary design of electromechanical actuators
|
Budinger, Marc
|
|
2014
|
228 |
9 |
p. 1598-1616
|
article
|
| 12 |
Parametric study of the effect of exothermic coating properties on blunt nose drag reduction in hypersonic flights
|
Tahsini, AmirMahdi
|
|
2014
|
228 |
9 |
p. 1461-1465
|
article
|
| 13 |
Preliminary reliability analysis of a high-altitude airship’s envelope
|
Liu, Jian
|
|
2014
|
228 |
9 |
p. 1648-1653
|
article
|
| 14 |
Research on advanced flight control methods based on actuator constraints for elastic model of hypersonic vehicle
|
Liu, Yan-bin
|
|
2014
|
228 |
9 |
p. 1627-1637
|
article
|
| 15 |
Shape optimization of airfoils in transonic flow using a multi-objective genetic algorithm
|
Chen, Xiaomin
|
|
2014
|
228 |
9 |
p. 1654-1667
|
article
|
| 16 |
Single sensor-based 3D feature point location for a small flying robot application using one camera
|
Shah, Syed Irtiza Ali
|
|
2014
|
228 |
9 |
p. 1668-1689
|
article
|
| 17 |
The birth of airplane stability theory
|
Magraner, JP
|
|
2014
|
228 |
9 |
p. 1498-1506
|
article
|
| 18 |
The design of nonsingular terminal sliding-mode feedback controller based on minimum sliding-mode error
|
Cao, Lu
|
|
2014
|
228 |
9 |
p. 1540-1561
|
article
|
| 19 |
The influence of wind shear to the performance of high-altitude solar-powered aircraft
|
Zhong, Gao Xian
|
|
2014
|
228 |
9 |
p. 1562-1573
|
article
|
Journal description