Design of an S-duct Intake for UAV Applications
AbstractPurpose - A numerical study is performed to design an S-Duct intake for UAV applications with good efficiency in a wide range of operating conditions.Design/methodology/approach - A...
View ArticleRobust Flutter Analysis and Control of a Wing
AbstractPurpose - This work presents a novel approach in aeroservoelastic analysis and control of a wing section with two control surfaces in leading-edge and trailing-edge using robust control. The...
View ArticleCollision Monitoring and Optimal Collision Avoidance Manoeuvre for Formation...
AbstractPurpose - This paper aims to evaluate the safety of formation flying satellites, and propose a method for practical collision monitoring and collision avoidance...
View ArticleA Nonlinear Stability Analysis of Elastic Flight Vehicle
AbstractPurpose - In this paper, a nonlinear model along with stability analysis of a flexible supersonic flight vehicle system is presented.Design/methodology/approach - The mathematical state space...
View ArticleInvestigation on instable current issue of scanning mechanism
AbstractPurpose - The purpose of this paper is to find the root cause of the current issue for a scan drive mechanism which is used to drive and to control the Microwave Radiometer Imager (MWRI)...
View ArticleEvaluation of Synthetic Jet Actuators Design Performance
AbstractPurpose - The purpose of this paper is to evaluate the synthetic jet actuator design's performance based on piezoelectric diaphragms that can appropriately use for flow separation...
View ArticleOptimal Formation Keeping Control in Missile Cooperative Engagement
AbstractPurpose - The purpose of this paper is to analyze the frame of a missile formation cooperative control system, and present an optimal keeping controller of a missile formation in the...
View ArticleStructural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor...
AbstractPurpose - This paper presents the development and application of a numerical formulation for the structural dynamics and aeroelastic analysis of new generation helicopter and tiltrotor rotor...
View ArticleDesign of an S-duct intake for UAV applications
AbstractPurpose – The purpose of this paper is to design an S-duct intake for unmanned aerial vehicles (UAVs) applications with good efficiency in a wide range of operating conditions....
View ArticleRobust flutter analysis and control of a wing
AbstractPurpose – The purpose of this paper is to present a novel approach in aeroservoelastic analysis and robust control of a wing section with two control surfaces in leading-edge and trailing-edge....
View ArticleCollision monitoring and optimal collision avoidance manoeuvre for formation...
AbstractPurpose – The purpose of this paper is to evaluate the safety of formation flying satellites, and propose a method for practical collision monitoring and collision avoidance manoeuvre....
View ArticleA nonlinear stability analysis of elastic flight vehicle
AbstractPurpose – The purpose of this paper is to present a nonlinear model along with stability analysis of a flexible supersonic flight vehicle system. Design/methodology/approach – The mathematical...
View ArticleInvestigation on instable current issue of scanning mechanism
AbstractPurpose – The purpose of this paper is to find the root cause of the current issue for a scan drive mechanism which is used to drive and to control the Microwave Radiometer Imager (MWRI)...
View ArticleEvaluation of synthetic jet actuators design performance
AbstractPurpose – The purpose of this paper is to evaluate the synthetic jet actuator design's performance based on piezoelectric diaphragms that can be appropriately used for flow separation control....
View ArticleOptimal formation keeping control in missile cooperative engagement
AbstractPurpose – The purpose of this paper is to analyze the frame of a missile formation cooperative control system, and present an optimal keeping controller of a missile formation in the...
View ArticleStructural-aeroelastic finite element modeling for advanced-geometry rotor...
AbstractPurpose – The purpose of this paper is to present the development and application of a numerical formulation for the structural dynamics and aeroelastic analysis of new generation helicopter...
View ArticleGravity gradient torque of spacecraft orbiting asteroids
AbstractPurpose - This paper presents a full fourth-order model of the gravity gradient torque of spacecraft around asteroids by taking into consideration of the inertia integrals of the spacecraft up...
View ArticlePenetration Trajectory Planning based on Radar Tracking Features for UAV
AbstractPurpose - The purpose of this paper is to plan the penetration trajectory of for unmanned aerial vehicle (UAV) in the presence of radar-guided surface to air missiles...
View ArticleA Directional Control System for UCAV Automatic Takeoff Roll
AbstractPurpose - The purpose of this paper is to develop a directional and roll control system for Unmanned combat air vehicle (UCAV) automatic takeoff roll, with the objective of keeping the UCAV...
View ArticleDynamics and Control for an In-plane Morphing Wing
AbstractPurpose - The paper aims to clarify the dynamic principle of internal structure of a complex morphing wing and control the wing to change configurations rapidly and smoothly. It includes...
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