no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
1 |
Active fault-tolerant satellite attitude control based on fault effect classification
|
Zhou, Jun |
|
2017 |
231 |
10 |
p. 1917-1934 |
article |
2 |
An improved footprint generation method for entry vehicles
|
Wang, Tao |
|
2017 |
231 |
10 |
p. 1951-1956 |
article |
3 |
Augmented predictive functional control for missile autopilot design
|
Guo, Jianguo |
|
2017 |
231 |
10 |
p. 1794-1803 |
article |
4 |
Dynamic combustion characteristics in a rectangular supersonic combustor with single-side expansion
|
Gao, Tianyun |
|
2017 |
231 |
10 |
p. 1862-1872 |
article |
5 |
Dynamics modeling and model selection of space debris removal via the Tethered Space Robot
|
Zhang, Fan |
|
2017 |
231 |
10 |
p. 1873-1897 |
article |
6 |
Lyapunov-based missile terminal guidance with short time convergence considering seeker’s first-order lag
|
Zheng, Duo |
|
2017 |
231 |
10 |
p. 1935-1950 |
article |
7 |
Modelling and analysis of coupled flap-lag-torsion vibration characteristics helicopter rotor blades
|
Castillo Pardo, Alejandro |
|
2017 |
231 |
10 |
p. 1804-1823 |
article |
8 |
Multidisciplinary design optimization architecture to concurrent design of satellite systems
|
Mohammad Zadeh, Parviz |
|
2017 |
231 |
10 |
p. 1898-1916 |
article |
9 |
Rapid generation of landing footprint based on geometry-predicted trajectory
|
Zhang, Yuan-Long |
|
2017 |
231 |
10 |
p. 1851-1861 |
article |
10 |
The effect of stiffness and geometric parameters on the nonlinear aeroelastic performance of high aspect ratio wings
|
Afonso, F |
|
2017 |
231 |
10 |
p. 1824-1850 |
article |
11 |
Trajectory optimization of unmanned aerial vehicle in dynamic soaring
|
Zhu, Bing-Jie |
|
2017 |
231 |
10 |
p. 1779-1793 |
article |
12 |
Utilizing ground-based LIDAR measurements to aid autonomous airdrop systems
|
Cacan, Martin |
|
2017 |
231 |
10 |
p. 1763-1778 |
article |