nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Aeroelastic numerical approach of a wing based on the finite element and boundary element methods
|
Dehkordi, Iman Roohi |
|
2013 |
227 |
5 |
p. 882-894 |
artikel |
2 |
Aircraft used as a sensor for atmospheric behaviour determination. Practical case: pressure estimation using automatic dependent surveillance-broadcast
|
Alarcón, José F Alonso |
|
2013 |
227 |
5 |
p. 778-797 |
artikel |
3 |
Analytical study of stationary temperature field in transpiration cooled porous wall
|
Zhukov, Victor P |
|
2013 |
227 |
5 |
p. 873-881 |
artikel |
4 |
Analytic solutions of optimal angularly constrained guidance for first-order lag system
|
Lee, Yong-In |
|
2013 |
227 |
5 |
p. 827-837 |
artikel |
5 |
A novel fault diagnosis approach based on environmental stress level evaluation
|
Deng, Guanqian |
|
2013 |
227 |
5 |
p. 816-826 |
artikel |
6 |
Decentralized robust coordinated control for formation flying spacecraft with coupled attitude and translational dynamics
|
Zhang, Bao-Qun |
|
2013 |
227 |
5 |
p. 798-815 |
artikel |
7 |
Frequency domain input identification for vibration testing of flexible structures
|
Ramkrishna, D |
|
2013 |
227 |
5 |
p. 838-856 |
artikel |
8 |
Fuzzy integral sliding mode based on backstepping control synthesis for an autonomous helicopter
|
Meguenni, Kadda Zemalache |
|
2013 |
227 |
5 |
p. 751-765 |
artikel |
9 |
Improving in-orbit responsiveness of low earth orbit sun-synchronous satellites by selection of ground segment location
|
Navabi, M |
|
2013 |
227 |
5 |
p. 766-777 |
artikel |
10 |
Librational characteristics of a dumbbell modeled tethered satellite under small, continuous, constant thrust
|
Zhao, Guowei |
|
2013 |
227 |
5 |
p. 857-872 |
artikel |
11 |
NOx, fuel consumption and time effects of flight path angle during descent
|
Turgut, Enis T |
|
2013 |
227 |
5 |
p. 737-750 |
artikel |