Volume 18, Issue 1 (4-1999)                   JCME 1999, 18(1): 113-125 | Back to browse issues page

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Abstract:   (2441 Views)
Guidance and control of aircraft in the landing phase imposes extra pilot work loads, hence application of automatic landing control systems is of great importance. In this study automatic landing control systems are introduced and an optimal landing control system is designed. The control system performance criteria are based on minimum control effort. The designed system is simulated for a transport category aircraft in accordance with FAR requirements. The results show that the designed system is completely capable of controlling the aircraft in its landing corridor.
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Type of Study: Research | Subject: General
Received: 2014/10/25