Developing Attitude Control for Suborbital Module Based on Cold Gas Thrusters and Using Quaternion Feedback
This paper presents the control design for large angle and high rotation rates maneuvers using reaction cold gas thrusters. Navigation system provides suborbital attitude changes in terms of quaternion. Cold gas thrusters with pulse-width pulse-frequency modulation provide nearly proportional contro...
| Main Authors: | , , |
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| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2013-04-01
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| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_14460_75eb7275366f4e5bae1639da0b9d7978.pdf |