>
Fa
|
Ar
|
En
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
Copyright 2023
Islamic World Science Citation Center
All Rights Reserved
