Abstract
Zhou et al in Ref.3 proposed an adaptive variable structure guidance law. In our opinion, it needs to be improved by using fuzzy control theory. Section 1 of the full paper discusses the factors that change continuously the angular velocity of the line of sight. Section 2 explains how we improve the adaptive variable structure guidance law in Ref.3; the result is that we add to it a term to compensate for the target maneuvers, this additional term being given by eq.(20) at the end of section 2. Section 3 designs this additional term by using fuzzy control theory. The simulation results, given in Fig.5 and Table 1 of the full paper, show preliminarily that our improved variable structure guidance law does suppress greatly the miss distance.
Original language | English |
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Pages (from-to) | 499-502 |
Number of pages | 4 |
Journal | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
Volume | 27 |
Issue number | 4 |
State | Published - Aug 2009 |
Keywords
- Fuzzy control
- Line of sight
- Missiles
- Target maneuver
- Variable structure control
- Variable structure guidance law