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علوم و فناوری فضایی
سال:2023 - دوره:16 - شماره:ویژه نامه
A New Adaptive Controller For The Three Axis Satellite Simulator Based On Continuous Time Delay Petri Nets Tool
- صفحه:25-38
Adaptive Generalized-Minimum-Variance Attitude Control Of A High Pointing-Accuracy Remote Sensing Satellite
- صفحه:1-23
Attitude Control Of Nanosatellite Using Optimal Quadratic Linear And Nonlinear Methods
- صفحه:51-64
Fmeca-Based Risk Assessment In Mono Propellant Hydrazine Propulsion System
- صفحه:39-50
Plant Germplasm And Extreme Conditions Of Outer Space
- صفحه:65-71
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