Optimal Nonlinear Dynamic Inversion-Based Flight Control System Design for an Aerospace Vehicle
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Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-15-1724-2_8
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1. Discrete-time attitude stabilization of reusable reentry vehicle by convex optimization;International Journal of Dynamics and Control;2021-01-01
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