001442637 000__ 11555cam\a2200613\a\4500 001442637 001__ 1442637 001442637 003__ OCoLC 001442637 005__ 20230310003428.0 001442637 006__ m\\\\\o\\d\\\\\\\\ 001442637 007__ cr\un\nnnunnun 001442637 008__ 211105s2022\\\\si\\\\\\o\\\\\100\0\eng\d 001442637 019__ $$a1283822246$$a1283950708$$a1294368327$$a1296665625 001442637 020__ $$a9789811674235$$q(electronic bk.) 001442637 020__ $$a981167423X$$q(electronic bk.) 001442637 020__ $$z9811674221 001442637 020__ $$z9789811674228 001442637 0247_ $$a10.1007/978-981-16-7423-5$$2doi 001442637 035__ $$aSP(OCoLC)1283140873 001442637 040__ $$aYDX$$beng$$epn$$cYDX$$dGW5XE$$dOCLCF$$dOCLCO$$dDCT$$dINU$$dDKU$$dOCLCO$$dOCLCQ$$dSFB$$dOCLCQ 001442637 049__ $$aISEA 001442637 050_4 $$aTL545 001442637 08204 $$a629.13$$223 001442637 1112_ $$aChina Aeronautical Science and Technology Conference$$n(5th :$$d2021 :$$cWu Zhen, Zhejiang Sheng, China) 001442637 24510 $$aProceedings of the 5th China Aeronautical Science and Technology Conference /$$cChinese Society of Aeronautics and Astronautics, editor. 001442637 260__ $$aSingapore :$$bSpringer,$$c[2022] 001442637 300__ $$a1 online resource 001442637 336__ $$atext$$btxt$$2rdacontent 001442637 337__ $$acomputer$$bc$$2rdamedia 001442637 338__ $$aonline resource$$bcr$$2rdacarrier 001442637 347__ $$atext file 001442637 347__ $$bPDF 001442637 4901_ $$aLecture notes in electrical engineering,$$x1876-1119 ;$$vv. 821 001442637 5050_ $$aIntro -- Contents -- Mechanical Modeling and Simulation for the Take-Off and Landing Performance Calculation of Low-Cost UAVs -- 1 Introduction -- 2 Concept and Approaches -- 2.1 Mechanical Modeling for Take-off Process -- 2.2 Mechanical Modeling for Landing Process -- 3 Results and Discussion -- 3.1 Parameters Setup -- 3.2 Results of Take-off Model -- 3.3 Computed Results of Landing Model -- 3.4 Discussion -- 4 Conclusions -- References -- Research on Dynamic Deformation Reconstruction Method of Full Size Wing Rocket Sled Based on Optical Fiber Strain -- 1 Introduction -- 2 Basic Principle of Deformation Monitoring Based on FBG -- 2.1 Fiber Bragg Grating Sensing Principle -- 2.2 Research on Subsection Fitting Deformation Monitoring Method -- 3 Overall Design of UAV Wing Deformation Reconstruction Experiment Using Rocket Sled -- 4 Test Results -- 4.1 Experimental Design -- 4.2 Analysis of Experimental Results -- 5 Conclusion -- References -- Strength Design and Research of Fuselage Opening Zone of Civil Aircraft -- 1 Introduction -- 2 Study on the Stiffness Analysis of the Open Area of the Fuselage -- 2.1 Computational Model -- 2.2 Lateral Bending Stiffness -- 2.3 Vertical bending stiffness -- 3 Conclusions -- References -- Characterization of the Rate-Dependent Behavior of Phenyl Silicone Rubber -- 1 Introduction -- 2 The Model -- 3 Experiments -- 3.1 Materials -- 3.2 Quasi-static Tests -- 3.3 High Rate Tests -- 4 Results and Discussions -- 4.1 Results of Tension Tests -- 4.2 Pure Elastic Stage of the Materials -- 4.3 Viscous-Hyperelastic Stage of the Materials -- 5 Conclusions -- References -- Design and Realization of Robotic Automatic Drilling &amp -- Riveting Controlling System for Single-Sided Fasteners -- 1 Introduction -- 2 System Overview -- 2.1 Structure of the Robotic Automatic Drilling &amp -- Riveting System. 001442637 5058_ $$a2.2 Design of the Control System -- 3 Implementation of the Control System -- 3.1 Communication Network of the Control System -- 3.2 Control Module of the End Effector -- 3.3 Normal Adjustment Algorithm -- 3.4 Drilling &amp -- Riveting Positioning Algorithm -- 4 Experiment -- 5 Conclusion -- References -- Experimental Study of Temperature on Eddy Current Sensor for Clearance Measurement -- 1 Introduction -- 2 Principle and Sensor -- 2.1 Principle of Eddy Current Measurement -- 2.2 Principle of Temperature Measurement -- 2.3 Sensor Design and Fabrication -- 3 Performance and Measurements -- 3.1 Calibration at Room Temperature -- 3.2 Effect of Temperature on Inductance and Resistance -- 4 Results Discussion -- 5 Conclusion -- References -- Numerical Investigation of Riblets on Rod-Airfoil Interaction Noise -- 1 Introduction -- 2 Numerical Methodology -- 3 Results and Discussion -- 4 Conclusions -- References -- System Level Study of Light Sport Aircraft with Conventional and Unconventional Propulsion Systems -- 1 Introduction -- 2 Background and Design Requirements -- 2.1 Background -- 2.2 Design Requirements -- 3 Methods -- 3.1 Overall Aircraft Design Methods -- 3.2 Electric Retrofit Design Method -- 4 Results -- 4.1 MDA Results for Conventional Propulsion Systems -- 4.2 Electric Retrofit Results -- 5 Conclusions -- References -- Research on Robust Scheduling Method Based on Operation Interval Relaxation -- 1 Introduction -- 2 Robust Scheduling Modeling Under Uncertain Delay -- 2.1 Robust Objective Function Selection -- 2.2 Problem Description and Modeling -- 3 Robust Scheduling Method Based on Operation Interval Relaxation -- 3.1 Method Description -- 3.2 Method Steps -- 3.3 Method Termination Conditions -- 4 Simulation -- 4.1 Experimental Design -- 4.2 Analysis of Results -- 5 Conclusions -- References. 001442637 5058_ $$aResearch on Out-of-Plane Shear Mechanical Properties of Damaged Composite T-joints -- 1 Introduction -- 2 Experiment -- 3 Numerical Simulation Method -- 3.1 CZM Constitutive Model -- 3.2 Finite Element Model -- 4 Results and Discussion -- 4.1 Model Validation -- 4.2 Structural Damage Failure Analysis -- 5 Conclusions -- References -- Hybrid Optimization of Arrival and Departure Flight Schedules -- 1 Introduction -- 2 Problem Description -- 3 Mathematical Model -- 3.1 Parameter Setting and Definition -- 3.2 Decision Variables -- 3.3 Objective Function -- 3.4 Constraints -- 3.5 Recurrence Formula of Optimized Takeoff/Landing Time -- 3.6 Interval Parameter Setting -- 4 Model Solving -- 5 Example Verification and Analysis -- References -- Research and Application of Simulation Technology in Airspace Capacity Assessment -- 1 Introduction -- 2 Simulation Method of Airspace Capacity Evaluation -- 2.1 Simulation Process -- 2.2 Evaluation Index Design -- 3 Principle -- 3.1 Principle of Flight Distance Calculation -- 3.2 Principle of Conflict Detection -- 3.3 Calculation Principle of ATC's Workload -- 4 Example Demonstration -- 4.1 Simulation Model Building -- 4.2 Analysis of Simulation Results -- 5 Conclusion -- References -- Research on Fault Diagnosis of INS/GNSS/CNS Integrated Navigation System Based on GA-BP Neural Network -- 1 Introduction -- 2 Principle of GA-BP Neural Network Algorithm -- 2.1 Principle and Structure of BP Neural Network -- 2.2 Principle and Structure of GA-BP Neural Network -- 2.3 Application of GA-BP Neural Network in Fault Diagnosis for INS/GNSS/CNS Integrated Navigation -- 3 Simulation and Analysis of Diagnosis for INS/GNSS/CNS Integrated Navigation -- 4 Conclusion -- References -- System Maintenance Method Based on the Mean Residual Life-Importance Measure -- 1 Introduction -- 2 Essential Technologies for Reliability Optimization. 001442637 5058_ $$a4 Conclusion -- References -- Assessment of Crash-Resistant Helicopter Fuel Tank with Composite Compartment Simulation for Drop Test -- 1 Introduction -- 2 Experimental Drop Test -- 2.1 Test Article -- 2.2 Test Facilities -- 2.3 Test Results -- 3 Finite Element Analysis -- 3.1 Fuel Bladders and Compartment -- 3.2 Crash Scenario -- 3.3 Analysis Result -- 4 Numerical-Test Correlation -- 5 Conclusions -- References -- Numerical Investigation and Analysis of Gas Leakage Process in High-Pressure Duct of Civil Aircraft -- 1 Introduction -- 2 Numerical Model -- 2.1 Research Objective -- 3 Numerical Model -- 4 Simulation Results and Discussions -- 4.1 Simulation Results -- 4.2 Discussions of Influence Factors -- References -- Research on Typical Joint Technology of Composite Stiffened Skin-Fuselage Frame -- 1 Introduction -- 2 Pull-Out Test of Composite T-joint -- 2.1 Preparation of Test Specimens -- 2.2 Pull-Out Testing -- 3 Pull-Out Failure Analysis of Composite T-joint -- 3.1 Delamination Failure Criterion -- 3.2 Adhesive Cohesive Behavior -- 3.3 Finite Element Simulation -- 3.4 Comparison of Test and Simulation Results -- 4 Conclusions -- References -- Fatigue Crack Growth Performance of Refilled Friction Stir Spot Welds in Similar and Dissimilar Aluminum Alloy Joints -- 1 Introduction -- 2 Experimental Procedures -- 2.1 Specimen Fabrication -- 2.2 FCG Test -- 3 Results and Discussion -- 3.1 Crack Growth Morphology -- 3.2 Crack Growth Lives -- 3.3 Crack Growth Rate -- 3.4 Fracture Surface -- 4 Conclusions -- References -- Clocking of Stators and Rotors in a Three-Stage Axial Turbine -- 1 Introduction -- 2 Description of Model and Computation Procedure -- 2.1 Geometry -- 2.2 The Scheme of Clocking Configuration -- 3 Clocking of a Single Row -- 3.1 Performance Variation -- 3.2 Relation of Wake Fragment and Leading Edge -- 3.3 Entropy Generation. 001442637 506__ $$aAccess limited to authorized users. 001442637 520__ $$aTo sort out the progress of aviation science and technology and industry, look forward to the future development trend, commend scientific and technological innovation achievements and talents, strengthen international cooperation, promote discipline exchanges, encourage scientific and technological innovation, and promote the development of aviation, the Chinese Aeronautical Society holds a China Aviation Science and Technology Conference every two years, which has been successfully held for four times and has become the highest level, largest scale, most influential and authoritative science and technology conference in the field of aviation in China. The 5th China Aviation Science and Technology Conference will be held in Wuzhen, Jiaxing City, Zhejiang Province in 2021, with the theme of "New Generation of Aviation Equipment and Technology", with academician Zhang Yanzhong as the chairman of the conference. This book contains original, peer-reviewed research papers from the conference. The topics covered include but are not limited to navigation, guidance and control technologies, key technologies for aircraft design and overall optimization, aviation test technologies, aviation airborne systems, electromechanical technologies, structural design, aerodynamics and flight mechanics, other related technologies, advanced aviation materials and manufacturing technologies, advanced aviation propulsion technologies, and civil aviation transportation. The papers presented here share the latest discoveries on aviation science and technology, making the book a valuable asset for researchers, engineers, and students 001442637 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed November 12, 2021). 001442637 650_0 $$aAeronautics$$vCongresses. 001442637 650_0 $$aAerospace engineering$$vCongresses. 001442637 650_6 $$aAéronautique$$vCongrès. 001442637 650_6 $$aAérospatiale (Ingénierie)$$vCongrès. 001442637 655_7 $$aConference papers and proceedings.$$2fast$$0(OCoLC)fst01423772 001442637 655_0 $$aElectronic books. 001442637 7102_ $$aZhongguo hang kong xue hui. 001442637 77608 $$iPrint version:$$aChina Aeronautical Science and Technology Conference (5th : 2021 : Wu Zhen, Zhejiang Sheng, China).$$tProceedings of the 5th China Aeronautical Science and Technology Conference.$$dSingapore : Springer, [2022]$$z9811674221$$z9789811674228$$w(OCoLC)1273078036 001442637 830_0 $$aLecture notes in electrical engineering ;$$vv. 821.$$x1876-1119 001442637 852__ $$bebk 001442637 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-981-16-7423-5$$zOnline Access$$91397441.1 001442637 909CO $$ooai:library.usi.edu:1442637$$pGLOBAL_SET 001442637 980__ $$aBIB 001442637 980__ $$aEBOOK 001442637 982__ $$aEbook 001442637 983__ $$aOnline 001442637 994__ $$a92$$bISE