Mr.Bailiang Lyu | Spacecraft Dynamics | Best Researcher Award
Mr.Bailiang Lyu , Northwestern Polytechnical University , China.
Mr.Bailiang Lyu is a dedicated Ph.D. candidate at Northwestern Polytechnical University (NPU) in China, specializing in flight vehicle design.
ย With a strong academic background in detection, guidance, and control technology, he has made significant contributions to spacecraft dynamics, control, and vibration mitigation.ย
ย His research focuses on advanced observer-based control methods, fault-tolerant systems, and intelligent algorithms for spacecraft stability.ย
ย Bailiang has published multiple high-impact journal articles and co-authored several patents in spacecraft control.ย
ย Beyond academia, he has actively participated in student services, demonstrating leadership and commitment.ย
ย Recognized with numerous scholarships and awards, he continues to excel in the field of astronautics.ย ![]()
Publication Profile
Scopus
Education & Experienceย 
ย Ph.D., Flight Vehicle Designย โ Northwestern Polytechnical University (2020โpresent)ย ![]()
ย B.S., Detection, Guidance & Control Technologyย โ Northwestern Polytechnical University (2020)ย ![]()
ย Ph.D. Candidateย at theย National Key Laboratory of Aerospace Flight Dynamicsย (2020โpresent)ย ![]()
ย Part-time Class Cadreย โ School of Astronautics (2016โ2020)ย ![]()
ย Student Envoy for Undergraduate Enrollmentย โ School of Astronauticsย ![]()
Suitability Summary
Mr.Bailiang Lyu is an candidate for the Best Researcher Award, demonstrating excellence in spacecraftdynamics, control engineering, and astronautics.ย
ย Hisย groundbreaking contributionsย to the field of flight vehicle design, particularly in the areas ofย fault-tolerant control, observer-based stabilization, and vibration mitigation for large-scale spacecraft, have had a significant impact on aerospace engineering.ย ![]()
Professional Developmentย 
Mr.Bailiang Lyu is deeply engaged in the advancement of spacecraft control systems and aerospace engineering.
ย His expertise lies in hybrid observer-based control strategies, fault-tolerant systems, and intelligent fuzzy logic applications for spacecraft stabilization.ย
ย His extensive research has been featured in renowned journals such asย Aerospace Science and Technology,ย IEEE Transactions on Aerospace and Electronic Systems, andย ISA Transactions.ย
Additionally, Bailiang has co-authored several patents related to spacecraft dynamics and control methodologies, highlighting his innovative contributions.ย
ย His professional journey includes active roles in student leadership, academic services, and participation in national aerospace competitions.ย
ย With a strong foundation in theoretical and applied research, he strives to push the boundaries of space technology, ensuring safer and more efficient space missions.ย ![]()
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Research Focusย 
Mr.Bailiang Lyuโs research centers on spacecraft dynamics, control, and vibration mitigation.ย
ย His work explores advancedย fault-tolerant control systems, intelligentย observer-based techniques, and innovativeย disturbance rejection mechanismsย to enhance spacecraft stability.ย ![]()
His studies inย multi-observer-based control,ย fuzzy logic algorithms, andย predictor-feedback methodsย contribute to developing moreย resilient spacecraft control systems.ย
ย Bailiang’s research extends toย hybrid rigid-flexible vibration isolation, optimizing large-scale spacecraft efficiency and longevity.ย
ย He integratesย machine learning,ย neural network-based disturbance observers, andย prescribed-time control strategiesย to refine space mission performance.ย ![]()
By addressing challenges likeย input saturation, orbital disturbances, and unbounded time delays, his work significantly advances modern astronautics.ย
ย His research directly supports futureย deep-space exploration missions, ensuring more robust and reliable spacecraft control technologies.ย ![]()
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Awards & Honorsย 
ย National Scholarshipย โ Northwestern Polytechnical University (2017)ย ![]()
ย 2nd Place in Advanced Mathematics Competitionย โ Shaanxi Province (2017)ย ![]()
ย Outstanding Student Awardย โ NPU (2017, 2018, 2019, 2022)ย ![]()
ย Guorui Scholarshipย โ Northwestern Polytechnical University (2022)ย ![]()
Publication Top Notes
ย Hybrid Nonfragile Intermediate Observer-Based TS Fuzzy Attitude Control for Flexible Spacecraft with Input Saturation
Authors:ย Bailiang Lyu, Chuang Liu, Xiaokui Yue
Journal:ย Aerospace Science and Technology
Volume & Issue:ย 128: 107753
Year:ย 2022
Cited by:ย TBDย ![]()
ย Constrained MultiโObserverโBased FaultโTolerant DisturbanceโRejection Control for Rigid Spacecraft
Authors:ย Bailiang Lyu, Xiaokui Yue, Chuang Liu
Journal:ย International Journal of Robust and Nonlinear Control
Volume & Issue:ย 32(14): 8102-8133
Year:ย 2022
Cited by:ย TBDย ![]()
ย Integrated Predictor-Observer Feedback Control for Vibration Mitigation of Large-Scale Spacecraft With Unbounded Input Time Delay
Authors:ย Bailiang Lyu, Chuang Liu, Xiaokui Yue
Journal:ย IEEE Transactions on Aerospace and Electronic Systems
Year:ย 2024
Cited by:ย TBDย ![]()
ย Parallel Layered Scheme-Based Integrated Orbit-Attitude-Vibration Coupled Dynamics and Control for Large-Scale Spacecraft
Authors:ย Bailiang Lyu, Xiaokui Yue, Chuang Liu
Journal:ย ISA Transactions
Year:ย 2025
Cited by:ย TBDย ![]()
ย Neural Network Disturbance Observer-Based Attitude Control for Flexible Spacecraft (in Chinese)
Authors:ย Xiaokui Yue, Bailiang Lyu, Chuang Liu, et al.
Journal:ย Aerospace Shanghai (Chinese & English)
Volume & Issue:ย 39(04): 58-65
Year:ย 2022
Cited by:ย TBDย ![]()
ย Fuzzy-Logic-Based Integrated Orbit-Attitude-Vibration Prescribed-Time Control for Large-Scale Flexible Spacecraft
Authors:ย Xiaokui Yue, Bailiang Lyu, Chuang Liu
Conference:ย International Conference on Computational & Experimental Engineering and Sciences
Publisher:ย Springer International Publishing
Pages:ย 839-849
Year:ย 2023
Cited by:ย TBDย ![]()