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journal of aerospace science and technology
سال:2023 - دوره:16 - شماره:2
a fuzzy fast terminal approach for tracking a probe around an asteroid
- صفحه:1-10
an enhanced lattice-boltzmann method for speeding numerical solutions
- صفحه:137-150
effects of harmonic control and dynamic twist on helicopter rotor performance in forward flight
- صفحه:95-113
guidance law design for the final stage of the orbit injection problem
- صفحه:61-73
integrated optimization of staging and trajectory of launch vehicles using b-spline curves
- صفحه:50-60
new guidance method for high altitude target based on constrained incremental predictive control
- صفحه:38-49
numerical study of flattened miniature heat pipe with hybrid porous wick and double heat sources
- صفحه:74-85
numerical study of the effect of tip clearance and rotor-stator distance on the performance of an axial turbine
- صفحه:124-136
on the effects of stiffness ratio in nonlinear aeroelastic stability of a folding wing
- صفحه:33-39
optimal round trip path-planning of an aerial robot by consideration of geometric constraints of obstacles
- صفحه:114-123
space robots formation control for large solar sail deployment
- صفحه:86-94
the success of the hybrid genetic and particle swarm algorithm for a return spacecraft from the atmosphere with an optimal trajectory design approach to reduce aerodynamic heat transfer
- صفحه:17-32
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