A new approach to mechatronics system design using hardware in the loop simulation

2002 ◽  
Author(s):  
D. Shetty ◽  
R.A. Kolk ◽  
J. Kondo ◽  
C. Campana
Keyword(s):  
System Design ◽  
Hardware In The Loop ◽  
New Approach

Optimization of significant insolation distribution parameters – A new approach towards BIPV system design

2010 ◽  
Vol 35 (10) ◽  
pp. 2182-2191 ◽  
Author(s):  
D. Paul ◽  
S.N. Mandal ◽  
D. Mukherjee ◽  
S.R. Bhadra Chaudhuri
Keyword(s):  
System Design ◽  
New Approach ◽  
Distribution Parameters

Adaptive Headlight System Design Using Hardware-In-The-Loop Simulation

2006 ◽  
Author(s):  
T. Hacibekir ◽  
S. Karaman ◽  
E. Kural ◽  
E.S. Ozturk ◽  
M. Demirci ◽  
...  
Keyword(s):  
System Design ◽  
Hardware In The Loop

A Meta-Heuristic with Ant Colony Approach to Complex System

2010 ◽  
Vol 26-28 ◽  
pp. 1147-1150
Author(s):  
Zong Li Liu ◽  
Jie Cao ◽  
Zhan Ting Yuan
Keyword(s):  
Complex System ◽  
System Design ◽  
Ant Colony ◽  
Pareto Optimal ◽  
Ant Colony Optimisation ◽  
New Approach ◽  
Pareto Optimal Set ◽  
Simulation Results ◽  
Optimal Set ◽  
Complex System Design

This paper proposes a new approach to determining the complex system design for a product mix comprising complex hierarchies of subassembly and components. Pareto Ant Colony Optimisation as an especially effective meta-heuristic for solving the problem of complex system design was introduced in this paper. A Pareto Optimal Set of complex system in which only the non dominated solutions allow ants to deposit pheromones over the time and cost pheromone matrices after certain generation runs. Simulation results show that the model for complex system and the hybrid algorithms are effective to the design of complex system.

EPISTLE: High lift system design for low-noise applied to a supersonic aircraft

2006 ◽  
Vol 110 (1107) ◽  
pp. 327-331 ◽  
Author(s):  
U. Herrmann
Keyword(s):  
System Design ◽  
Aircraft Design ◽  
Reynolds Numbers ◽  
Low Noise ◽  
High Lift ◽  
New Approach ◽  
Low Speed ◽  
Supersonic Aircraft ◽  
Preliminary Aircraft Design ◽  
High Reynolds

Abstract A new approach for low-drag high-lift system design based on the application of viscous flow solvers was developed in the EC research project EPISTLE. Two high-lift systems for a supersonic commercial transport aircraft (SCT) wing were designed, manufactured and wind-tunnel tested. The predicted large drag reductions were fully confirmed by tests at high Reynolds numbers. These drag reductions significantly reduce the low-speed noise of future SCT configurations. This was estimated by preliminary aircraft design tools. Low-speed noise reduction by aerodynamic means is obtained, as effective high-lift systems enable these aircraft to climb faster.

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