MODERN AND CONVENTIONAL RAFT GUI IDDANCE AND CONTROL PROBLEM IN AIRAFT GUIDED MISSILES | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 27, Volume 5, ASAT CONFERENCE 4 - 6 May 1993, CAIRO, May 1993, Page 315-324 PDF (1.96 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.1993.25634 | ||||
 View on SCiNiTO | ||||
| Authors | ||||
| Wagih M. M.1; Wahid Kassem2 | ||||
| 1Ph. D. student, Air Defence Forces. | ||||
| 2A. Prof. Chair Of Elect. Equip. And Armament Of A/C, Cairo M.T.C. | ||||
| Abstract | ||||
| The increased accuracy requirements, more dynamic battlefield tactics of modern warfare, arbitrary and unpredictable nature of target maneuverability render classical guidance laws (such as proportional navigation) unsatisfactory in many applications. The solution involves a critical comparison between our current modern approach and the classical approach to missile guidance and control. Single plane analysis is used throughout and simulation result shows that even an accelerating target can be intercepted with shorter miss distance and less time duration for homing in spite of the dynamic lags in the target tracker and the missile dynamics. | ||||
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