Numerical Survey of Vibrational Model for Third Aircraft based on HR Suspension System Actuator Using Two Bee Algorithm Objective Functions

This research explains airplane model with two vertical vibrations for airframe and landing gear system. The purpose of this work is to advance vibrational model for study of adjustable vibration absorber and to plan Proportional-Integration-Derivative approach for adapting semi active control force. The coefficients of this method are modified as stated by Bee multiobjective optimization using minimizing accelerations and impact forces as objective functions. The consequences implies that the semi active shock absorber system based on artificial Bee colony improves passengers and ride comfort and fatigue life of fuselage, shock strut and tyre by reducing movement of body, suspension system and impact load in an important way compared to passive performance during touchdown phase with various sink speeds and runway surfaces for robustness and sensitivity investigation of optimization performance.

[1]  Liu Hui,et al.  Application of High-speed Solenoid Valve to the Semi-active Control of Landing Gear , 2008 .

[2]  Duc Truong Pham,et al.  APPLICATION OF THE BEES ALGORITHM TO THE TRAINING OF RADIAL BASIS FUNCTION NETWORKS FOR CONTROL CHART PATTERN RECOGNITION , 2006 .

[3]  S Sivakumar,et al.  Mathematical model and vibration analysis of aircraft with active landing gears , 2015 .

[4]  H. D. Carden,et al.  Analytical investigation of the landing dynamics of a large airplane with a load-control system in the main landing gear , 1979 .

[5]  Ali Reza Toloei,et al.  Vibration Control of Aircraft Semi-Active Suspension System using PID-Bees Technique , 2014 .

[6]  Duc Truong Pham,et al.  OPTIMIZATION OF THE WEIGHTS OF MULTI-LAYERED PERCEPTIONS USING THE BEES ALGORITHM , 2006 .

[7]  D. Pham,et al.  THE BEES ALGORITHM, A NOVEL TOOL FOR COMPLEX OPTIMISATION PROBLEMS , 2006 .

[8]  Duc Truong Pham,et al.  PRELIMINARY DESIGN USING THE BEES ALGORITHM , 2007 .

[9]  Ali Reza Toloei,et al.  Oscillation Control of Aircraft Shock Absorber Subsystem Using Intelligent Active Performance and Optimized Classical Techniques Under Sine Wave Runway Excitation (TECHNICAL NOTE) , 2016 .

[10]  Lucas G. Horta,et al.  Modeling and Validation of a Navy A6-Intruder Actively Controlled Landing Gear System , 1999 .

[11]  S. Sivakumar,et al.  Aircraft Random Vibration Analysis Using Active Landing Gears , 2015 .

[12]  D.T. Pham,et al.  Application of the Bees Algorithm to the Training of Learning Vector Quantisation Networks for Control Chart Pattern Recognition , 2006, 2006 2nd International Conference on Information & Communication Technologies.

[13]  W. G. Price,et al.  An investigation of an active landing gear system to reduce aircraft vibrations caused by landing impacts and runway excitations , 2008 .

[14]  I. Ross,et al.  Application of active control landing gear technology to the A-10 aircraft , 1983 .

[15]  Klaus Koenig.  Aircraft Dynamic Response to Damaged and Repaired Runways. , 1982 .

[16]  N. S. Currey,et al.  Aircraft landing gear design : principles and practices , 1988 .

[17]  I Pritchard Jocelyn.  An Overview of Landing Gear Dynamics , 1999 .

[18]  James N. Daniels,et al.  A method for landing gear modeling and simulation with experimental validation , 1996 .

[19]  Ali Reza Toloei,et al.  MATHEMATICAL MODEL AND VIBRATION ANALYSIS OF AIRCRAFT WITH ACTIVE LANDING GEAR SYSTEM USING LINEAR QUADRATIC REGULATOR TECHNIQUE , 2016 .

[20]  Ali Reza Toloei,et al.  Application of Active Suspension System to Reduce Aircraft Vibration using PID Technique and Bees Algorithm , 2014 .

[21]  Ali Reza Toloei,et al.  OPTIMIZED FUZZY LOGIC FOR NONLINEAR VIBRATION CONTROL OF AIRCRAFT SEMI-ACTIVE SHOCK ABSORBER WITH INPUT CONSTRAINT (TECHNICAL NOTE) , 2016 .

[22]  Robert H. Daugherty,et al.  F-106B airplane active control landing gear drop test performance , 1990 .