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Improving the Orbit Injection Accuracy of a Launch Vehicle by Using a Mode-Switching Strategy for a Dual-Axis

Jun Li1,2, Shifeng Zhang1,2, Zhenlin Ma1,2

  • 1College of Aerospace and Engineering, National University of Defense Technology, Changsha 410073, China.

Sensors (Basel, Switzerland)
|January 11, 2025
PubMed

Keywords:
mode-switching strategyorbit injection accuracyrotational inertial navigation system

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