Supported by the National Natural Science Foundation of China(No.52005441);Natural Science Foundation of Zhejiang Province(No.LQ21E050017);Young Elite Scientist Sponsorship Program by CAST(No.2022QNRC001);State Key Laboratory of Mechanical System and Vibration(No.MSV202316);"Pioneer"and"Leading Goose"R&D Program of Zhejiang Province(Nos.2022C01122,2022C01132);the Fundamental Research Funds for the Provincial Universities of Zhejiang(No.RFA2023007);the Research Project of ZJUT(No.GYY-ZH2023075).
Hydraulic circuits with high speed on/off valve(HSV)for servo control have become commonplace in aerospace.However,the individual valve that is not volume-optimized results in a large total size of hydraulic control s...
In order to obtain the optimized aircraft design concept which meets the increasingly complex operation environment at the conceptual design stage,System-of-systems(So S)engineering must be considered.This paper propo...
the Natural Science Foundation of Liaoning (No. 20180550824)。
The composite leaf spring landing gear of an electric aircraft is optimized.With the strength and workability as constraints and the minimum structural weight as an objective,the two-stage optimization of the leaf spr...
National Key Research and Development Program(2017YFB1102800);NSFC for Excellent Young Scholars(11722219);National Natural Science Foundation of China(11772258,51790171,5171101743)。
Flexible chiral honeycomb cores generally exhibit nonlinear elastic properties due to large geometric deformation.The effective elastic moduli and Poisson's ratio typically vary with an increase in deformation.Here,th...
This paper develops a Quantum-inspired Genetic Algorithm(QGA) to find the sets of optimal parameters for the wind disturbance alleviation Flight Control System(FCS). To search the problem domain more evenly and unifor...
supported by the National Natural Science Foundation of China (No. 11502211)
In aerodynamic optimization, global optimization methods such as genetic algorithms are preferred in many cases because of their advantage on reaching global optimum. However,for complex problems in which large number...
co-supported by the National Natural Science Foundation of China (Nos. 51405460, 11372128 and 51175244);National Safety Academic Foundation of China (No. U1730129);the Collaborative Innovation Center of Advanced Aero-Engine, Jiangsu Province Key Laboratory of Aerospace Power System,the Key Laboratory of Aero-Engine Thermal Environment and Structure, Ministry of Industry and Information Technology
A novel approach to identify the crystal orientation of turbine blades with anisotropy materials is proposed. Based on enhanced mode basis, with the main advantages of its efficiency,accuracy and general applicability...
co-supported by the National Natural Science Foundation of China (Nos. 51675047, 11372036, and 51105040);the Aeronautical Science Foundation of China (No. 2015ZA72004)
This paper presents a novel multiple Unmanned Aerial Vehicles(UAVs) reconnaissance task allocation model for heterogeneous targets and an effective genetic algorithm to optimize UAVs' task sequence. Heterogeneous t...
co-supported by National Natural Science Foundation of China(Grant No.51505015,51575019);the National Basic Research Program of China(No.2014CB046402);CAST-BISEE Innovation Foundation of China
Harmonic drives have various distinctive advantages and are widely used in space drive mechanisms. Accelerated life test (ALT) is commonly conducted to shorten test time and reduce associated costs. An appropriate A...
co-supported by the National High-tech Research and Development Program of China (Grant No.2011AA110101);the Foundation for Innovative Research Groups of the National Natural Science Foundation of China (Grant No. 60921001);China Scholarship Council
Conflict avoidance (CA) plays a crucial role in guaranteeing the airspace safety. The cur- rent approaches, mostly focusing on a short-term situation which eliminates conflicts via local adjust- ment, cannot provide...