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Design of Autoland Controller Functions with Multiobjective Optimization
2006
Journal of Guidance Control and Dynamics
The application of multi-objective optimization to the design of longitudinal automatic landing control laws for a civil aircraft is discussed. The control laws consist of a stability and command augmentation, a speed / flight path tracking, a glide slope guidance, and a flare function. Multi-objective optimization is used to synthesize the free parameters in these controller functions. Performance criteria are thereby computed from linear as well as nonlinear analysis (eg. simulations,
doi:10.2514/1.8797
fatcat:pdeb64d6ancsnijc6b4ijggheq