| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A coupled free-wake/panel method for rotor/fuselage/empennage aerodynamic interaction and helicopter trims
|
Cao, Yihua
|
|
2015
|
229 |
3 |
p. 435-444
|
artikel
|
| 2 |
An improved decentralized model for sensor fault detection and isolation demonstrated on an airplane system
|
Wang, Jianchen
|
|
2015
|
229 |
3 |
p. 423-434
|
artikel
|
| 3 |
Attitude control of a small-scale helicopter based on backstepping
|
Tang, Shuai
|
|
2015
|
229 |
3 |
p. 502-516
|
artikel
|
| 4 |
Design and qualification of a supersonic wind tunnel for induced boundary layer transition research
|
Bottini, H
|
|
2015
|
229 |
3 |
p. 562-578
|
artikel
|
| 5 |
Electrical load-sizing methodology to aid conceptual and preliminary design of large commercial aircraft
|
Seresinhe, Ravinka
|
|
2015
|
229 |
3 |
p. 445-466
|
artikel
|
| 6 |
Influence of aeroelastic control reversal problem in the airplane lateral stability modes
|
Rose, J Bruce Ralphin
|
|
2015
|
229 |
3 |
p. 517-533
|
artikel
|
| 7 |
Leakage analysis and ground tests of the O-type rubber ring seal applied in lunar sample return devices
|
Zhang, Bin
|
|
2015
|
229 |
3 |
p. 479-491
|
artikel
|
| 8 |
Nonlinear relative dynamics of Lorentz spacecraft about J2-perturbed orbit
|
Huang, Xu
|
|
2015
|
229 |
3 |
p. 467-478
|
artikel
|
| 9 |
Research of a fuzzy global sliding mode control scheme: A stability control scheme for anti-aircraft missile with swing nozzle thrust vector control
|
Liu, Xiaodong
|
|
2015
|
229 |
3 |
p. 554-561
|
artikel
|
| 10 |
Research on the method of suppressing sun and moon's interference on infrared conical earth sensor
|
Xianbin, Hu
|
|
2015
|
229 |
3 |
p. 399-406
|
artikel
|
| 11 |
Sinusoidal function weighted optimal guidance laws
|
Lee, Chang-Hun
|
|
2015
|
229 |
3 |
p. 534-542
|
artikel
|
| 12 |
Testability demonstration for a flight control system based on sequential probability ratio test method
|
Qiu, Jing
|
|
2015
|
229 |
3 |
p. 492-501
|
artikel
|
| 13 |
Three-axis L1 adaptive attitude control of spacecraft using solar radiation pressure
|
Lee, Keum W
|
|
2015
|
229 |
3 |
p. 407-422
|
artikel
|
| 14 |
Vortex flow hypothesis for a yawed rotor blade in reverse flow*
|
Mayo, Michael
|
|
2015
|
229 |
3 |
p. 543-553
|
artikel
|
Tijdschrift beschrijving