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                             15 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 An adaptive wavelet collocation method for solving optimal control problem Zhang, Qingbin
2015
229 9 p. 1640-1649
artikel
2 A new homing guidance law to reduce sensitivity on initial heading errors Shin, Hyo-Sang
2015
229 9 p. 1740-1753
artikel
3 A new star pattern identification technique using an improved triangle algorithm Li, Xin-lu
2015
229 9 p. 1730-1739
artikel
4 Application of an automated aircraft architecture generation and analysis tool to unmanned aerial vehicle subsystem design Judt, David M
2015
229 9 p. 1690-1708
artikel
5 A study on the thrust vector control using a bypass flow passage Deng, R
2015
229 9 p. 1722-1729
artikel
6 Concept description and assessment of the main features of a geared intercooled reversed flow core engine Camilleri, William
2015
229 9 p. 1631-1639
artikel
7 Control system design for hypersonic reentry vehicle driven by aerosurfaces and reaction control system Cai, Gaohua
2015
229 9 p. 1575-1587
artikel
8 Integrated guidance and control based on block backstepping sliding mode and dynamic control allocation Guo, Chao
2015
229 9 p. 1559-1574
artikel
9 Modification of Leishman–Beddoes model incorporating with a new trailing-edge vortex model Wang, Qing
2015
229 9 p. 1606-1615
artikel
10 Nonlinear adaptive trajectory tracking control for a quad-rotor with parametric uncertainty Sun, Liang
2015
229 9 p. 1709-1721
artikel
11 Nonlinear aerodynamic model identification using empirical mode decomposition Bagherzadeh, SA
2015
229 9 p. 1588-1605
artikel
12 Researches on inverse simulation’s applications in teleoperation rendezvous and docking based on hyper-ellipsoidal restricted model predictive control for inverse simulation structure Zhou, Wanmeng
2015
229 9 p. 1675-1689
artikel
13 Reynolds averaged Navier-Stokes simulations of compressible mixing layers of similar and dissimilar gases: Performance of k–ɛ turbulence model Javed, Afroz
2015
229 9 p. 1650-1660
artikel
14 Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach Zhao, Yao
2015
229 9 p. 1616-1630
artikel
15 Variable structure and variable coefficient proportional-integral-derivative control to prevent actuator saturation of yaw movement for a coaxial eight-rotor unmanned aerial vehicle Peng, Cheng
2015
229 9 p. 1661-1674
artikel
                             15 gevonden resultaten
 
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