关键词: 飞行器控制、导航技术, 机载布撒器, 发射扇面角, 进入

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.

Key words: control and navigation technology of aerocraft, airborne dispenser, sector angular, entry angular, circular-navigation-guidance, integrated guidance law