Launch window for manned Moon-to-Earth trajectories
AbstractPurpose - The paper aims to establish an orbital launch window for manned Moon-to-Earth trajectories to support China’s manned lunar landing mission requirements of high-latitude landing and...
View ArticleCluster Flight Orbit Design Method for Fractionated Spacecraft
AbstractPurpose - The purpose of this paper is to propose an intuitive and effective cluster flight orbit design method for fractionated spacecraft.Design/methodology/approach - Based on the concept of...
View ArticleAttitude Cooperative Control of Spacecraft Formation via Output-feedback
AbstractPurpose - This paper aims to propose a decentralized output feedback controller for cooperative attitude regulation of spacecraft formation in absence of angular velocity...
View ArticleRotor Unsteady Aerodynamics Model Using an Efficient Free-Vortex Method
AbstractPurpose - The purpose of this paper is to present and validate an efficient time-marching free-vortex method for rotor wake analysis and study the rotor wake dynamics in transient and...
View ArticleStability Analysis of Aeroelastic Systems Based on Aeroelastic FRF and...
AbstractPurpose - The purpose of this paper is to analyze the stability of aeroelastic systems using aeroelastic frequency response function (FRF).Design/methodology/approach - The proposed technique...
View ArticleEvaluation on Net Strength and Arresting Performance of Aircraft Arresting...
AbstractPurpose - The objective of this paper is to provide an effective way to evaluate structure strength margin of AAS (Aircraft Arresting System) barrier net and efficiency of its control...
View ArticleIntegrity monitoring using ERAIM for GNSS/Inertial system
AbstractPurpose - The objective of this paper is to develop an integrity monitoring method using ERAIM (Extended Receiver Autonomous Integrity Monitoring) for the GNSS/Inertial integrated navigation...
View ArticleFriction and wear behaviors of aircraft brake linings material
AbstractPurpose - The objective of this paper is to produce and investigate a reliable and effective aircraft brake lining material.Design/methodology/approach - Four different Cu based brake lining...
View ArticleDesign 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 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)...
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