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Control failure of the roll-isolated inertial navigation system under large pitch angle |
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| Institution: | 1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;2. Xi’an Modern Control and Technology Institute, Xi’an 710065, China;3. Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China |
| Abstract: | |
| Keywords: | Spinning vehicle Strap-down inertial navigation system (SINS) Roll-isolated control Control failure Large pitch angle |
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