| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A coordinated turn controller for a fixed-wing aircraft
|
Corona-Sánchez, José J
|
|
2019
|
233 |
5 |
p. 1728-1740
|
artikel
|
| 2 |
A distribution model of the GNSS code noise and multipath error considering both elevation angle and orbit type
|
Fan, Guochao
|
|
2019
|
233 |
5 |
p. 1900-1915
|
artikel
|
| 3 |
A 3D pitch and impact-angle constrained guidance scheme
|
Varma, S Aditya
|
|
2019
|
233 |
5 |
p. 1571-1584
|
artikel
|
| 4 |
A quadratic homotopy method for fuel-optimal low-thrust trajectory design
|
Pan, Binfeng
|
|
2019
|
233 |
5 |
p. 1741-1757
|
artikel
|
| 5 |
Aspects of aero-engine nacelle drag
|
Robinson, Matthew
|
|
2019
|
233 |
5 |
p. 1667-1682
|
artikel
|
| 6 |
A winding machine for polarized wire grid of microwave radiometer calibration
|
Hu, Yong
|
|
2019
|
233 |
5 |
p. 1916-1925
|
artikel
|
| 7 |
Comparison between bolt clamping force and composite patches for repairing aircraft structures of aluminum alloy 2024-T3
|
Maleki, HN
|
|
2019
|
233 |
5 |
p. 1758-1771
|
artikel
|
| 8 |
Design optimization of a thrust chamber using a mass-based model to improve the geometrical and performance parameters of low-thrust space propulsion systems
|
Shafaee, Maziar
|
|
2019
|
233 |
5 |
p. 1820-1837
|
artikel
|
| 9 |
Development of a new tool for constrained conflict resolution
|
Han, Yun-xiang
|
|
2019
|
233 |
5 |
p. 1683-1694
|
artikel
|
| 10 |
Dynamic response analysis of aero hydraulic pipeline system under pump fluid pressure fluctuation
|
Gao, Pei-xin
|
|
2019
|
233 |
5 |
p. 1585-1595
|
artikel
|
| 11 |
Effects of revolute clearance joint on the dynamic behavior of a planar space arm system
|
Miao, Huihui
|
|
2019
|
233 |
5 |
p. 1629-1644
|
artikel
|
| 12 |
Experimental study on axially non-uniform clearances in a linear turbine cascade with a cavity squealer tip
|
Chen, Shaowen
|
|
2019
|
233 |
5 |
p. 1645-1655
|
artikel
|
| 13 |
Film cooling optimization on leading edge gas turbine blade using differential evolution
|
García, Juan C
|
|
2019
|
233 |
5 |
p. 1656-1666
|
artikel
|
| 14 |
Finite element analysis of solar sail force model with mission application
|
Boni, Luisa
|
|
2019
|
233 |
5 |
p. 1838-1846
|
artikel
|
| 15 |
Flight test of flying-wing type unmanned aerial vehicle with partial wing-loss
|
Kim, Kijoon
|
|
2019
|
233 |
5 |
p. 1611-1628
|
artikel
|
| 16 |
Identification of spin maneuver aerodynamic nonlinear model by applying ensemble empirical mode decomposition and extended multipoint modeling
|
Mokhtari, MA
|
|
2019
|
233 |
5 |
p. 1865-1878
|
artikel
|
| 17 |
Large deformation bending responses of nanotube-reinforced polymer composite panel structure: Numerical and experimental analyses
|
Mehar, Kulmani
|
|
2019
|
233 |
5 |
p. 1695-1704
|
artikel
|
| 18 |
Linear-parameter-varying-based adaptive sliding mode control with bounded L2 gain performance for a morphing aircraft
|
Wen, Nuan
|
|
2019
|
233 |
5 |
p. 1847-1864
|
artikel
|
| 19 |
Nonlinear system controllability analysis and autopilot design for bank-to-turn aircraft with two flaps
|
Dong, Jinlu
|
|
2019
|
233 |
5 |
p. 1772-1783
|
artikel
|
| 20 |
Nonsingular adaptive-gain super-twisting guidance with an impact angle constraint
|
Li, Guofei
|
|
2019
|
233 |
5 |
p. 1705-1714
|
artikel
|
| 21 |
Planar path following nonlinear controller design for an autonomous airship
|
Zhou, Wei-xiang
|
|
2019
|
233 |
5 |
p. 1879-1899
|
artikel
|
| 22 |
Quasi-continuous high-order sliding mode control-based fault-tolerant control for hypersonic flight vehicle via neural network observer
|
Cheng, Zian
|
|
2019
|
233 |
5 |
p. 1784-1800
|
artikel
|
| 23 |
Reviewer List 2019
|
|
|
2019
|
233 |
5 |
p. 1935-1940
|
artikel
|
| 24 |
Robust output feedback trajectory tracking for quadrotors
|
Shi, Xiling
|
|
2019
|
233 |
5 |
p. 1596-1610
|
artikel
|
| 25 |
The establishment and verification of kinematic equation of all link centroid of the manipulator mounted on a satellite
|
Zhang, Hongwen
|
|
2019
|
233 |
5 |
p. 1801-1819
|
artikel
|
| 26 |
Three-dimensional aero-thermo-elasticity analysis of functionally graded cylindrical shell panels
|
Fazilati, Jamshid
|
|
2019
|
233 |
5 |
p. 1715-1727
|
artikel
|
| 27 |
Three-dimensional relative reachable domain with initial state uncertainty in Gaussian distribution
|
Wen, Changxuan
|
|
2019
|
233 |
5 |
p. 1555-1570
|
artikel
|
| 28 |
Unmanned air vehicles for targeting tasks
|
Ashokkumar, Chimpalthradi R
|
|
2019
|
233 |
5 |
p. 1926-1934
|
artikel
|
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