제어로봇시스템학회:학술대회논문집
- 2002.10a
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- Pages.82.2-82
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- 2002
Guidance Law for a Flight Vehicle after Burnout
- Dohi, Naoto (Nat'l Defense Academy, JAPAN) ;
- Baba, Yoriaki (Nat'l Defense Academy, JAPAN) ;
- Takano, Hiroyuki (Nat'l Defense Academy, JAPAN)
- Published : 2002.10.01
Abstract
The new guidance law for a missile with the varying velocity after the rocket motor burned out is presented. This guidance is mechanized by combining the proportional navigation and the pure pursuit navigation. Some simulations are performed and then the simulation results show that the guidance law presented is effective even if the vehicle speed decreases significantly and has higher off-boresight ability than the proportional navigation.
Keywords