A Guidance Control Method for Imaging Air-to-Ground Missiles

Precise attacking of the vital regions of the threatening targets can be achieved by using the imaging air-to-ground missiles (AGMs), and a guidance control method suitable for the stable control of the imaging AGM is proposed in this paper. Components of the guidance control system are determined on the basis of the guidance property analysis of the imaging seekers, and the calculation method of target pointing is given based on the inertial navigation system (INS). Stable missile body control is realized by fusing tilt stability control, attitude control, height control, gravity compensation control, environmental adoption compensation control, and impact angle constraint control together. Experimental results on real collected data have verified the effectiveness of the proposed method.