In a close air support situation, the pilot can locate and off-boresight target the enemy, come around and release weapons, and thus minimize exposure to ground threats.

This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.

The stability of a kind of missile guidance system is analyzed, and the effect of perturbation of radome boresight error slope a on the stability is investigated.