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- W2366613662 abstract "Taking aim at the existences of sector angle launching and entry angle constraint in the airborne dispense,the integrated guidance law was proposed by the smooth characteristic of arc trajectory and combining the pursuit guidance law with the circular-navigation-guidance(CNG)law,with maximal needed overload almost does not change with the launching and entry conditions at the small enough sector angle.The simulated results demonstrate that the integrated guidance law can reduce the maximal needed overload and enhance the adaptability of airborne dispenser to the launch and entry conditions." @default.
- W2366613662 created "2016-06-24" @default.
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- W2366613662 date "2010-01-01" @default.
- W2366613662 modified "2023-09-23" @default.
- W2366613662 title "Research on Integrated Guidance Law with the Entry Angle Constraint" @default.
- W2366613662 hasPublicationYear "2010" @default.
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