Aerodynamic control analysis in a canard configuration for a surface-to-surface missile

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The modern battlefield requires highly accurate missiles, which has led to the modification of unguided missiles into guided versions. This paper presents the process of adapting an unguided missile with a range of 40 km into a guided version using a canard control system. A key aspect of the upgrade was the development of a control system that allows the trajectory to be corrected after crossing the apex of the flight path, particularly during the descent phase. This paper discusses the design details and application of a two-channel control system (pitch and yaw) in which the control signals are synchronized with the speed of the projectile. Mathematical modelling and numerical simulations have shown that, with appropriate control parameters, a zero mean control force can be achieved, leading to trajectory stabilization and minimized aiming errors. The proposed solution provides a basis for further research and dynamic field tests and can contribute to the development of precision guidance technology for surface-to-surface missiles.

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