Modeling and Simulation Analysis of a Kind of High Speed Aircraft
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Jing Li, Hui Li and Junwei Lei
High speed aircraft is researched widely by researchers because of its high value of application in the weapon design and military purpose. The modeling and simulation of high speed model is research and the open loop response is researched. At last, detailed numerical simulation was done with a real simplified pitch channel system model to testify the ability of aircraft body.
Disturbance, Observer, Backstepping, Missile, Control system