Days Hours Minutes Seconds

The International Conference on
Aerospace System Science and
Engineering

JULY 06-07, 2023

SHANGHAI, CHINA

Program

Program

July 6th, 2023

Day 1

Opening Ceremony

08:40-10:20 (GMT+8)

Rm 114, Aerospace Bldg.

8:40-8:50

WELCOME REMARKS

8:50-9:00

GROUP PHOTO

9:00-9:30

Keynote Speech:

HYBRID LES-RANS WITH AN ADAPTIVE DOWNSTREAM RANS MODEL

Tom Shih

9:30-10:00

Keynote Speech:

NONLINEAR H-INFINITY ATTITUDE CONTROL USING MODIFIED RODRIGUES PARAMETERS

Chris Damaren

10:00-10:20

BREAK

Track 1

10:20-12:00 (GMT+8)

Rm. 114, Aerospace Bldg.

Session Chair: Chris Damaren

10:20-10:50

Invited Speech:

COORDINATED CONTROL FOR AUTONOMOUS DRONE SAMPLING APPLICATIONS

Hugh Liu

10:50-11:20

Invited Speech:

MULTIPLE-TO-ONE ORBITAL PURSUIT: A COMPUTATIONAL GAME APPROACH

Chaoyong Li

11:20-11:40

INVESTIGATION INTO PROVISIONS AND VALIDATION FOR COCKPIT SMOKE EVACUATION ON CIVIL AIRCRAFT

P0363

11:40-12:00

A SPACECRAFT ATTITUDE CONTROL METHOD BASED ON NEURAL NETWORK AND FUZZY-PD

P0364

LUNCH

 Center for Academic Activities, SJTU Minhang Campus

Track 1

13:30-17:05 (GMT+8)

Rm. 114, Aerospace Bldg.

Session Chair: Hugh Liu

13:30-13:50

A THREE-DIMENSIONAL ANGLE CONSTRAINED GUIDANCE LAW FOR HYPERSONIC VEHICLE WITH APPLICATION TO SALVO ATTACK SCENARIO

P0366

13:50-14:10

FAULT DIAGNOSIS BASED ON FEATURE ENHANCEMENT MULTISCALE NETWORK UNDER NONSTATIONARY CONDITIONS

P0386

14:10-14:30

COOPERATIVE ORGANIZATION AND OPERATION MECHANISM BASED ON OPERATIONAL INTENTION ENVIRONMENTTARGE

P0408

14:30-14:50

RESEARCH ON ALTITUDE ADJUSTMENT PERFORMANCE OF STRATOSPHERIC AIRSHIP BASED ON THERMODYNAMIC-DYNAMIC-PRESSURE COUPLED

P0410

14:50-15:10

AN APPROACH TO ASSESSING THE SAFETY OF AN AIRCRAFT AND ITS SYSTEMS

P0421

15:10-15:30

DYNAMIC MODELING OF THE ELECTRICAL ACTUATION SYSTEM OF THE HYPERSONIC AIRCRAFT CONSIDERING THE TEMPERATURE EFFECTS

P0389

BREAK

15:45-16:05

RESEARCH ON CAPABILITY CATALOG GENERATION OF UAV INTELLI-GENT SYSTEM BASED ON DODAF

P0391

16:05-16:25

THE ROLE OF DIGITAL TWINS OF AVIATION PRODUCTS IN END-TO-END LIFECYCLE MANAGEMENT TECHNOLOGIES

P0395

16:25-16:45

SYSML-BASED APPROACH FOR FUNCTIONAL QUANTITATIVE MODELING OF CIVIL AIRCRAFT SYSTEMS

P0367

16:45-17:05

RESEARCH ON MAGICGRID-BASED REQUIREMENTS DEVELOPMENT PROCESS OF FLIGHT CONTROL SYSTEM

P0376

 
 

 

Track 2

10:20-11:40 (GMT+8)

Rm. 228, Aerospace Bldg.

Session Chair: Tom Shih

10:20-10:50

Invited Speech:

HYDROGEN ROTATING DETONATION COMBUSTION TECHNOLOGY AND APPLICATIONS

Bing Wang

10:50-11:20

Invited Speech:

STUDY ON THE BLOW-OFF CHARACTERISTICS OF BLUFF-BODY STABILIZED PREMIXED FLAME UTILIZING HIGH-SPEED PIV/OH-PLIF MEASUREMENTS

Yi Gao

11:20-11:40

ANALYSIS OF IMPACT PROPERTIES OF NANOCOMPOSITES AT MICRON SCALE

P0383

LUNCH

 Center for Academic Activities, SJTU Minhang Campus

Track 2

13:30-17:05 (GMT+8)

Rm. 228, Aerospace Bldg.

Session Chair: George Zhu

13:30-13:50

INVESTIGATION OF THE 2-D DISTRIBUTION FORM OF BEARING STRESS IN A SINGLE-BOLT SINGLE-SHEAR METAL-COMPOSITE HYBRID JOINT

P0413

13:50-14:10

FINITE STATE MACHINE AND ULTRASONIC RANGING-BASED APPROACH FOR AUTOMATIC GRASPING BY FLIGHT MANIPULATOR

P0385

14:10-14:30

MODELING METHODS OF REPAIRED POLYMER COMPOSITE MATERIAL SPECIMENS

P0396

14:30-14:50

ELECTRIC BRAKE ACTUATING MECHANISM DESIGN FOR COMMERCIAL AIRCRAFT BASED ON AN ENERGY ANALYSIS METHOD

P0403

14:50-15:10

LONG-ENDURANCE MARS EXPLORATION FLYING VEHICLE: A PROJECT BRIEF

P0405

15:10-15:30

PARAMETRIC OPTIMIZATION OF AERODYNAMIC LAYOUT OF A SUPERSONIC PASSENGER AIRCRAFT

P0409

BREAK

15:45-16:05

OPTIMIZATION OF THE COMPOSITE STRUCTURE MONITORING SYSTEM FOR OPERATIONAL DAMAGE REGISTRATION LAYOUT

P0418

16:05-16:25

THE IMPACT OF BLEEDING SLOT ANGLES ON THE PERFORMANCE OF A COMPRESSOR

P0414

16:25-16:45

DAMAGE PREDICTION AND FAILURE MODE ANALYSIS OF COMPOSITE AEROENGINE BLADE IMPACTED BY THE BREAKSTONE

P0417

16:45-17:05

ISSUES OF APPLICATION OF AUTOMATED LAYOUT METHODS TAKING INTO ACCOUNT DESIGN AND TECHNOLOGICAL FEATURES IN THE PRODUCTION OF PARTS AND ASSEMBLIES MADE OF POLYMER COMPOSITES

P0419

July 7th, 2023

Day 2

Track 1

Rm. 114, Aerospace Bldg.

9:00-12:15 (GMT+8)

Session Chair: Haichao Hong

9:00-9:30

Invited Speech:

CONVEX OPTIMIZATION IN AEROSPACE GUIDANCE AND CONTROL

Ping Lu

9:30-10:00

Invited Speech:

MODEL-FREE FAULT-TOLERANT CONTROL OF SPACECRAFT

Qiang Shen

10:00-10:20

PROCESS APPROACH AS A TOOL OF THE KNOWLEDGE-INTENSIVE INDUSTRY ORGANIZATION MANAGEMENT SYSTEM

P0453

BREAK

10:35-10:55

ROBUST CONTROL DESIGN FOR ZERO-SUM DIFFERENTIAL GAMES PROBLEM

P0380

10:55-11:15

LPV ROBUST FILTER BASED FAULT DIAGNOSIS METHOD FOR AEROENGINE CONTROL SYSTEM

P0411

11:15-11:35

A DATA-DRIVEN DYNAMIC THRESHOLDING AND HEALTH INDEX CONSTRUCTION FOR IMPROVED DIAGNOSIS AND PROGNOSIS OF ENGINE BLEED AIR SYSTEM

P0390

11:35-11:55

AIRPORT COLLABORATIVE DECISION-MAKING IN SINGLE PILOT OPERA-TIONS OF COMMERCIAL AIRCRAFT

P0388

11:55-12:15

RESEARCH ON THE CONTRIBUTION RATE OF SHIPBOARD MANNED/UNMANNED AERIAL VEHICLE COOPERATIVE OPERATION BASED ON WARGAME DATA MINING

P0404

LUNCH

 Center for Academic Activities, SJTU Minhang Campus

Track 1

Rm. 114, Aerospace Bldg.

13:30-17:15 (GMT+8)

Session Chair: Ping Lu

13:30-14:00

Invited Speech:

QUANTIFYING SAFE DYNAMIC PERFORMANCE BOUNDARIES FOR EVTOL AIRCRAFT

Haichao Hong

14:00-14:20

USE OF A PREDICTIVE DISPLAY TO ENSURE A TARGET LEVEL OF SAFETY AND PILOTING ACCURACY WHILE REDUCING THE RANGE OF THE FINAL APPROACH FIX IN A CIVIL AIRCRAFT

P0435

14:20-14:40

EXPERIMENTAL STUDY ON SINGLE NOZZLE PERFORMANCE OF HEAVY GAS TURBINE COMBUSTOR

P0378

14:40-15:00

ANALYSIS OF THE INFLUENCE OF TOTAL PRESSURE ERROR 0N AIR DATA  CALIBRATION

P0379

15:00-15:20

INFLUENCE OF RADIUS OF MICROPHONE ARRAY ON VIRTUAL ROTATING ARRAY BEAMFORMING FOR ROTATING NOISE SOURCE LOCALIZATION

P0371

15:20-15:40

EFFECT OF THE INCOMING BOUNDARY LAYER THICKNESS ON THE CAVITY FLOW CHARACTERISTIC WITH THE DELAYED DETACHED EDDY SIMULATION

P0369

BREAK

15:55-16:15

APPLICATION INDUSTRY 4.0 DIGITAL TECHNOLOGIES TO QUALITY MANAGEMENT IN MODERN AVIATION MANUFACTURE

P0452

16:15-16:35

A FINITE ELEMENT METHOD OF RESEARCH ON TRANSVERSE MECHAN-ICAL PROPERTIES OF FIBER-REINFORCED COMPOSITES WITH RANDOM MATRIX VOID DEFECTS

P0373

16:35-16:55

A REVIEW OF SOME KEY ISSUES IN CFD-BASED THROUGHFLOW SIMULATION

P0375

16:55-17:15

HYBRID OPTIMIZATION OF CURVATURE CONTINUOUS STACKING LINE ON THE HIGHLY-LOADED DIFFUSER CASCADE

P0392

       
 

Track 2

9:00-12:15 (GMT+8)

Rm. 228, Aerospace Bldg.

Session Chair: Yi Gao

9:00-9:30

Invited Speech:

GLOBAL CHALLENGES FOR SUPERSONIC AVIATION

Dmitry Strelets

9:30-10:00

Invited Speech:

PATH PLANNING AND VISUAL SERVO FOR AUTONOMOUS FREE-FLOATING ROBOTIC MANIPULATORS BY REINFORCEMENT LEARNING

George Zhu

10:00-10:20

MULTI-OBJECTIVE OPTIMIZATION DESIGN OF LABYRINTH SEAL OF SHROUDED STATOR CAVITY IN A LOW-SPEED RESEARCH COMPRESSOR

P0431

BREAK

10:35-10:55

DETERMINATION OF THE OPTIMAL WALL RUN-OUT ANGLE OF THE COMPOSITE WING STRINGER

P0423

10:55-11:15

DECONVOLUTION OF MODE COMPOSITION BEAMFORMING FOR ROTATING SOURCE LOCALIZATION

P0437

11:15-11:35

THERMAL CONDUCTIVITY OF FUNCTIONAL FIBROUS INHOMOGENEOUS MATERIALS

 P0441

11:35-11:55

PARAMETRIC INVESTIGATION OF A COMPOSITE QUASI-ISOTROPIC PANEL THICKNESS INFLUENCE ON THE BARELY VISIBLE IMPACT DAMAGE THRESHOLD VALUE

        P0424

11:55-12:15

STRUCTURAL CHARACTERISTICS AND INFLUENCING FACTORS ANALYSIS OF SEMI-RIGID STRATOSPHERIC AIRSHIP

P0445

LUNCH

 Center for Academic Activities, SJTU Minhang Campus

Track 2

13:30-17:45 (GMT+8)

Rm. 228, Aerospace Bldg.

Session Chair: Qiang Shen

13:30-13:50

ANGLE OF ATTACK OF THE AIRCRAFT CALIBRATION

P0362

13:50-14:10

INTEGRATED FATIGUE LIFE COMPUTATIONAL ANALYSIS OF THE COMPOSITE STRUCTURE

P0446

14:10-14:30

MATHEMATICAL MODELING OF DEFECTS INITIALIZATION FROM VERY HIGH CYCLE FATIGUE

P0463

14:30-14:50

FORMATION OF THE LAYOUT OF A SUPERSONIC PASSENGER AIRCRAFT IN ORDER TO ENSURE A LOW LEVEL OF SONIC BOOM

P0420

14:50-15:10

IMPLEMENTATION OF OPTIMAL SIZE-WEIGHT PROJECT WITH RESTRICTIONS ON REFINED BUCKLING THEORY FOR STRUCTURALLY ANISOTROPIC AIRCRAFT PANELS MADE OF COMPOSITE MATERIALS

P0440

15:10-15:30

A PROMISING HYBRID COMPOSITE MATERIAL FILLED WITH SMA WIRES

P0425

BREAK

15:45-16:05

STUDY ON THE HYSTERETIC THERMAL STRESS IN METAL-COMPOSITE HYBRID STRUCTURES

P0427

16:05-16:25

DESIGN PARAMETERS DETERMINATION OF A LIGHT TRANSPORT AIRCRAFT FOR OPERATION IN REGIONS OF SOUTHEAST ASIA

P0429

16:25-16:45

DESIGN OF THE MAIN LANDING GEAR OF A REGIONAL AIRCRAFT USING A PROMISING NUMERICAL MESHFREE METHOD

P0456

16:45-17:05

INVESTIGATION OF THE POTENTIAL APPLICATION OF FUNDAMENTALLY NEW FOAM PLASTIC MATERIALS IN THE MANUFACTURE OF POWER ELEMENTS OF AIRCRAFT STRUCTURES FROM PCM BY VACUUM INFUSION

P0466

17:05-17:25

PROGRESS IN BASIC AND APPLIED STUDIES ON THE PILOT-AIRCRAFT SYSTEM

P0434

17:25-17:45

NUMERICAL INVESTIGATION OF DIFFUSER CURVILINEAR MERIDIONAL SHAPE ON CENTRIFUGAL COMPRESSOR STAGE PERFORMANCE

P0443

Banquet and Closing Ceremony

18:30-20:00 (GMT+8)

Baijinhanjue Hotel, Rm. 180 (No. 1577, Humin Rd., Minhang District)