Planning test points for highly constrained flight tests is a lengthy and iterative process which requires a structured, methodical approach using scientific test and analysis techniques (STAT) including: design theory, multi-objective optimization, and uncertainty analysis. Flight test engineers can spend anywhere from a week to a month determining ideal test points, only to have unforeseen problems arise during the week of testing that can invalidate these points. Genetic algorithms can play a key role in point selection for two common types of tests: model verification and validation (V&V) testing and operational test (OT) design. This paper outlines the methodology behind building a program to quickly identify a set of optimal test poin...
The flight control law clearance problem can be formulated as a robustness analysis problem, where ...
Aircraft design is a complex and lengthy process dependent upon many competing disciplinary analyses...
Due the fact that aircraft structures work in an environment with lots of dynamic forces, it is of v...
Planning test points for highly constrained flight tests is a lengthy and iterative process which re...
The growing development of numerical simulation in aviation industry raises the issue of the quality...
In this paper we present a computational methodology to solve the problem of the proper design of th...
Airborne surveillance systems have multiple sensors and communication links on board a suitable plat...
Commercial airline optimisation of operation flight plan requires a list of waypoints or Navaids and...
Increase in fuel costs have pushed airlines to look for ways to cut costs substantially. One area wh...
In this paper we present a computational methodology to solve the problem of the proper design of th...
A computational methodology for an experimental design problem based on the concept of potential and...
In this paper we study the problem of the design of the test matrix for an envelope expansion test c...
A computational methodology for designing an experimental test matrix is presented based on the conc...
Purpose – The purpose of this paper is to present an original design procedure for a flight control ...
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 ...
Aircraft design is a complex and lengthy process dependent upon many competing disciplinary analyses...
Due the fact that aircraft structures work in an environment with lots of dynamic forces, it is of v...
Planning test points for highly constrained flight tests is a lengthy and iterative process which re...
The growing development of numerical simulation in aviation industry raises the issue of the quality...
In this paper we present a computational methodology to solve the problem of the proper design of th...
Airborne surveillance systems have multiple sensors and communication links on board a suitable plat...
Commercial airline optimisation of operation flight plan requires a list of waypoints or Navaids and...
Increase in fuel costs have pushed airlines to look for ways to cut costs substantially. One area wh...
In this paper we present a computational methodology to solve the problem of the proper design of th...
A computational methodology for an experimental design problem based on the concept of potential and...
In this paper we study the problem of the design of the test matrix for an envelope expansion test c...
A computational methodology for designing an experimental test matrix is presented based on the conc...
Purpose – The purpose of this paper is to present an original design procedure for a flight control ...
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 ...
Aircraft design is a complex and lengthy process dependent upon many competing disciplinary analyses...
Due the fact that aircraft structures work in an environment with lots of dynamic forces, it is of v...