Program
JULY 06-07, 2023
SHANGHAI, CHINA
July 6th, 2023 Day 1 |
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Opening Ceremony 08:40-10:20 (GMT+8) Rm 114, Aerospace Bldg. |
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8:40-8:50 |
WELCOME REMARKS |
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8:50-9:00 |
GROUP PHOTO |
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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 |
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Track 1 10:20-12:00 (GMT+8) Rm. 114, Aerospace Bldg. Session Chair: Chris Damaren |
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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 |
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Track 1 13:30-17:05 (GMT+8) Rm. 114, Aerospace Bldg. Session Chair: Hugh Liu |
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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 |
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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 |
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10:20-10:50 |
Invited Speech: HYDROGEN ROTATING DETONATION COMBUSTION TECHNOLOGY AND APPLICATIONS |
Bing Wang |
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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 |
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11:20-11:40 |
ANALYSIS OF IMPACT PROPERTIES OF NANOCOMPOSITES AT MICRON SCALE |
P0383 |
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LUNCH Center for Academic Activities, SJTU Minhang Campus |
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Track 2 13:30-17:05 (GMT+8) Rm. 228, Aerospace Bldg. Session Chair: George Zhu |
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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 |
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13:50-14:10 |
FINITE STATE MACHINE AND ULTRASONIC RANGING-BASED APPROACH FOR AUTOMATIC GRASPING BY FLIGHT MANIPULATOR |
P0385 |
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14:10-14:30 |
MODELING METHODS OF REPAIRED POLYMER COMPOSITE MATERIAL SPECIMENS |
P0396 |
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14:30-14:50 |
ELECTRIC BRAKE ACTUATING MECHANISM DESIGN FOR COMMERCIAL AIRCRAFT BASED ON AN ENERGY ANALYSIS METHOD |
P0403 |
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14:50-15:10 |
LONG-ENDURANCE MARS EXPLORATION FLYING VEHICLE: A PROJECT BRIEF |
P0405 |
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15:10-15:30 |
PARAMETRIC OPTIMIZATION OF AERODYNAMIC LAYOUT OF A SUPERSONIC PASSENGER AIRCRAFT |
P0409 |
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BREAK |
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15:45-16:05 |
OPTIMIZATION OF THE COMPOSITE STRUCTURE MONITORING SYSTEM FOR OPERATIONAL DAMAGE REGISTRATION LAYOUT |
P0418 |
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16:05-16:25 |
THE IMPACT OF BLEEDING SLOT ANGLES ON THE PERFORMANCE OF A COMPRESSOR |
P0414 |
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16:25-16:45 |
DAMAGE PREDICTION AND FAILURE MODE ANALYSIS OF COMPOSITE AEROENGINE BLADE IMPACTED BY THE BREAKSTONE |
P0417 |
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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 |
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July 7th, 2023 Day 2 |
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Track 1 Rm. 114, Aerospace Bldg. 9:00-12:15 (GMT+8) Session Chair: Haichao Hong |
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9:00-9:30 |
Invited Speech: CONVEX OPTIMIZATION IN AEROSPACE GUIDANCE AND CONTROL |
Ping Lu |
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9:30-10:00 |
Invited Speech: MODEL-FREE FAULT-TOLERANT CONTROL OF SPACECRAFT |
Qiang Shen |
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10:00-10:20 |
PROCESS APPROACH AS A TOOL OF THE KNOWLEDGE-INTENSIVE INDUSTRY ORGANIZATION MANAGEMENT SYSTEM |
P0453 |
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BREAK |
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10:35-10:55 |
ROBUST CONTROL DESIGN FOR ZERO-SUM DIFFERENTIAL GAMES PROBLEM |
P0380 |
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10:55-11:15 |
LPV ROBUST FILTER BASED FAULT DIAGNOSIS METHOD FOR AEROENGINE CONTROL SYSTEM |
P0411 |
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11:15-11:35 |
A DATA-DRIVEN DYNAMIC THRESHOLDING AND HEALTH INDEX CONSTRUCTION FOR IMPROVED DIAGNOSIS AND PROGNOSIS OF ENGINE BLEED AIR SYSTEM |
P0390 |
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11:35-11:55 |
AIRPORT COLLABORATIVE DECISION-MAKING IN SINGLE PILOT OPERA-TIONS OF COMMERCIAL AIRCRAFT |
P0388 |
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11:55-12:15 |
RESEARCH ON THE CONTRIBUTION RATE OF SHIPBOARD MANNED/UNMANNED AERIAL VEHICLE COOPERATIVE OPERATION BASED ON WARGAME DATA MINING |
P0404 |
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LUNCH Center for Academic Activities, SJTU Minhang Campus |
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Track 1 Rm. 114, Aerospace Bldg. 13:30-17:15 (GMT+8) Session Chair: Ping Lu |
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13:30-14:00 |
Invited Speech: QUANTIFYING SAFE DYNAMIC PERFORMANCE BOUNDARIES FOR EVTOL AIRCRAFT |
Haichao Hong |
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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 |
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14:20-14:40 |
EXPERIMENTAL STUDY ON SINGLE NOZZLE PERFORMANCE OF HEAVY GAS TURBINE COMBUSTOR |
P0378 |
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14:40-15:00 |
ANALYSIS OF THE INFLUENCE OF TOTAL PRESSURE ERROR 0N AIR DATA CALIBRATION |
P0379 |
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15:00-15:20 |
INFLUENCE OF RADIUS OF MICROPHONE ARRAY ON VIRTUAL ROTATING ARRAY BEAMFORMING FOR ROTATING NOISE SOURCE LOCALIZATION |
P0371 |
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15:20-15:40 |
EFFECT OF THE INCOMING BOUNDARY LAYER THICKNESS ON THE CAVITY FLOW CHARACTERISTIC WITH THE DELAYED DETACHED EDDY SIMULATION |
P0369 |
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BREAK |
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15:55-16:15 |
APPLICATION INDUSTRY 4.0 DIGITAL TECHNOLOGIES TO QUALITY MANAGEMENT IN MODERN AVIATION MANUFACTURE |
P0452 |
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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 |
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16:35-16:55 |
A REVIEW OF SOME KEY ISSUES IN CFD-BASED THROUGHFLOW SIMULATION |
P0375 |
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16:55-17:15 |
HYBRID OPTIMIZATION OF CURVATURE CONTINUOUS STACKING LINE ON THE HIGHLY-LOADED DIFFUSER CASCADE |
P0392 |
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Track 2 9:00-12:15 (GMT+8) Rm. 228, Aerospace Bldg. Session Chair: Yi Gao |
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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 |
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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 |
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Track 2 13:30-17:45 (GMT+8) Rm. 228, Aerospace Bldg. Session Chair: Qiang Shen |
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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 |
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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) |