Satyanarayana, G and Sarma, IG and Prasad, UR (2007) Optimal control for the rolling pullout maneuver of a modern fighter aircraft. In: 1975 IEEE Conference on Decision and Control including the 14th Symposium on Adaptive Processes, Dec. 1975.
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Optimal control laws are obtained for the elevator and the ailerons for a modern fighter aircraft in a rolling pullout maneuver. The problem is solved for three flight conditions using the conjugate gradient method.
|Item Type:||Conference Paper|
|Additional Information:||Copyright 2007 IEEE. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||27 Dec 2011 08:28|
|Last Modified:||27 Dec 2011 08:28|
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