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علوم و فناوری فضایی
سال:2018 - دوره:11 - شماره:2
finite time guidance law to intercept desired los angle using ntsm control
- صفحه:1-10
lowprofile helical antenna for space application
- صفحه:55-59
lyapunovbasedadaptive smoothsecondorder sliding mode guidance law with proving finite time stability
- صفحه:33-39
numerical simulation and optimization of forced convection heat transfer of magnetic nanofluid in a channel in the presence of a nonuniform magnetic field
- صفحه:11-19
optimal mission design for moon exploration expedition
- صفحه:47-53
robust switching surfaces sliding mode guidance for terminal rendezvous in near circular orbit
- صفحه:21-31
velocity and body rate control of a spacecraft using robust passivitybased control
- صفحه:41-46
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