1979
DOI: 10.1016/0005-1098(79)90007-4
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Application of multiobjective optimization in aircraft control systems design

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Cited by 41 publications
(17 citation statements)
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“…Furthermore, two more important parameters describe the behavior of an airplane in flying conditions. The first is the sideslip angle β that is the rotation angle of the nose of the airplane due to the relative wind, see [63]. The second one is the bank angle φ , that is a metric related to the speed (and performance) of the airplane and is measured in (aperiodic) degrees, see [21] for details.…”
Section: Preference Articulation In the Design Of A Fighter Vehicle Cmentioning
confidence: 99%
“…Furthermore, two more important parameters describe the behavior of an airplane in flying conditions. The first is the sideslip angle β that is the rotation angle of the nose of the airplane due to the relative wind, see [63]. The second one is the bank angle φ , that is a metric related to the speed (and performance) of the airplane and is measured in (aperiodic) degrees, see [21] for details.…”
Section: Preference Articulation In the Design Of A Fighter Vehicle Cmentioning
confidence: 99%
“…In this work, only the lateral/ directional motion control is considered. A state equation representing the dynamic motion of an aircraft is expressed as follows [57][58][59][60] where x = { , , , } , is the sideslip, a velocity in direction, is the yaw rate, rate of change of rotation about the -axis, is the roll rate, rate of change of rotation about the -axis, is the bank angle, rotation about the -axis, A is the kinetic energy matrix, B is Coriolis matrix, u = { } is the control vector, is the aileron deflection, and is the rudder deflection.…”
Section: Flight Dynamic Control Optimisation Problemmentioning
confidence: 99%
“…More details about this aircraft dynamic model can be found in [58][59][60]. To handle the constraints, the penalty function which was presented in [61] is used.…”
Section: Flight Dynamic Control Optimisation Problemmentioning
confidence: 99%
“…Previous applications of multiple-objective decision making in the analysis of engineering systems included the choice of location for an underground power plant and the design of an aircraft lateral control system. In (24] the authors point out that multiple-objective analysis provides the designer with a high level of flexibility in choosing between various design options. This has been demonstrated in the design of lateral control systems for a heavy re-entry vehicle and a fighter aircraft [24].…”
mentioning
confidence: 99%
“…In (24] the authors point out that multiple-objective analysis provides the designer with a high level of flexibility in choosing between various design options. This has been demonstrated in the design of lateral control systems for a heavy re-entry vehicle and a fighter aircraft [24].…”
mentioning
confidence: 99%