Cottrell, R. G., "Optimal Intercept Guidance for Short-Range Tactical Missiles," AIAA Journal, Vol.9, No.7, 1971, pp. 1414-1415. Home/Search Document Not in Database Summary Related Articles |
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Autopilot Design for BTT Missiles Using Receding Horizon.. - Myung-Joon Kimy (1997) (Correct)
....they deal with zero steady state error for constant guidance commands. For arbitrary guidance commands, these approaches may yield tracking errors between commanded outputs and achieved outputs. The tracking errors are possibly a major factor contributing to excessive terminal miss distances [11]. Generally the tracking performance for arbitrary reference commands is known to be good in predictive controls when finite future reference commands are available in advance. Predictive control has been applied successfully in many control applications and its good tracking performance has been ....
Cottrell, R. G., "Optimal Intercept Guidance for Short-Range Tactical Missiles," AIAA Journal, Vol.9, No.7, 1971, pp. 1414-1415.
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