제어로봇시스템학회:학술대회논문집
- 1995.10a
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- Pages.283-286
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- 1995
Effects of time-to-go freezing on PN guidance loop stability
- Rew, Dong-Young (Dept. of Aerospace Eng., KAIST) ;
- Tahk, Min-Jae (Dept. of Aerospace Eng., KAIST)
- Published : 1995.10.01
Abstract
Due to finite bandwidth of missile dynamics, guidance commands in PN guidance tend to diverage as the missile approaches to the target. In this paper, a new method based on the short-time stability theorem is introduced to extend the stability region.