This book summarizes the main achievements of the EC funded 6th Framework Program project COFCLUO – Clearance of Flight Control Laws Using Optimization. This project successfully contributed to the achievement of a top-level objective to meet society’s needs for a more efficient, safer and environmentally friendly air transport by providing new techniques and tools for the clearance of flight control laws. This is an important part of the certification and qualification process of an aircraft – a costly and time-consuming process for the aeronautical industry. The overall objective of the COFCLUO project was to develop and apply optimization techniques to the clearance of flight control laws in order to improve efficiency and reliability....
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
The article explains the use of modifications the classical method PSO to optimize the training pilo...
The flight control law design assessment problem can be formulated as a robustness analysis problem,...
The flight control law clearance problem can be formulated as a robustness analysis problem, where ...
This chapter describes the development of evolutionary and deterministic global optimisation methods...
In this thesis, optimization is used to improve the performance of aircraft. The focus is on operati...
The basic feature of the optimisation-based clearance approach is to reformulate the clearance probl...
The design of flight control laws (FCLs) for automatic and manual (augmented) control of aircraft is...
In this report we describe the clearance criteria which are intended to serve for robustness analys...
The application of two evolutionary optimization methods, namely, differential evolution and genetic...
This paper describes the development and current status of a fully automated aircraft model integrat...
In the course of the FaUSST project scope, a versatile and flexible method for the synthesis of flig...
In this report we describe the ¯rst version of the criteria library for the op- timization based cl...
This article is placed here with permission from the Royal Aeronautical Society - Copyright @ 2009 R...
The usage of light utility high aspect ratio aircraft with payload up to 350kg is deemed to be an ec...
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
The article explains the use of modifications the classical method PSO to optimize the training pilo...
The flight control law design assessment problem can be formulated as a robustness analysis problem,...
The flight control law clearance problem can be formulated as a robustness analysis problem, where ...
This chapter describes the development of evolutionary and deterministic global optimisation methods...
In this thesis, optimization is used to improve the performance of aircraft. The focus is on operati...
The basic feature of the optimisation-based clearance approach is to reformulate the clearance probl...
The design of flight control laws (FCLs) for automatic and manual (augmented) control of aircraft is...
In this report we describe the clearance criteria which are intended to serve for robustness analys...
The application of two evolutionary optimization methods, namely, differential evolution and genetic...
This paper describes the development and current status of a fully automated aircraft model integrat...
In the course of the FaUSST project scope, a versatile and flexible method for the synthesis of flig...
In this report we describe the ¯rst version of the criteria library for the op- timization based cl...
This article is placed here with permission from the Royal Aeronautical Society - Copyright @ 2009 R...
The usage of light utility high aspect ratio aircraft with payload up to 350kg is deemed to be an ec...
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
The article explains the use of modifications the classical method PSO to optimize the training pilo...
The flight control law design assessment problem can be formulated as a robustness analysis problem,...