Personal information

Verified email addresses

Activities

Employment (1)

Beihang University: Beijing, CN

professor (School of Aeronautic Science and Engineering)
Employment
Source: Self-asserted source
Lixin Wang

Works (50 of 123)

Items per page:
Page 1 of 3

Design of Ice Tolerance Flight Envelope Protection Control System for UAV Based on LSTM Neural Network for Detecting Icing Severity

Drones
2025-01-16 | Journal article
Contributors: Ting Yue; Xianlong Wang; Bo Wang; Shang Tai; Hailiang Liu; Lixin Wang; Feihong Jiang
Source: check_circle
Crossref
grade
Preferred source (of 2)‎

Identification of aircraft longitudinal aerodynamic parameters using an online corrective test for wind tunnel virtual flight

Chinese Journal of Aeronautics
2024-09 | Journal article
Contributors: Shang TAI; Chen BU; Yanling WANG; Ting YUE; Hailiang LIU; Lixin WANG
Source: check_circle
Crossref

Sliding Mode Flight Control Law Design Requirements for Oblique Wing Aircraft Based on Perturbation Theory

Aerospace
2024-05-06 | Journal article
Contributors: Lixin Wang; Xun Sun; Hailiang Liu; Jingzhong Ma; Wenyuan Cheng; Shang Tai; Yun Zhu; Ting Yue
Source: check_circle
Crossref
grade
Preferred source (of 2)‎

Flight Dynamics Modeling and Aerodynamic Parameter Identification of Four-Degree-of-Freedom Virtual Flight Test

AIAA Journal
2023-05 | Journal article
Contributors: Shang Tai; Lixin Wang; Yanling Wang; Chen Bu; Ting Yue
Source: check_circle
Crossref

Research on Dynamic Characteristics Analysis and Control Law Design Method of Model Aircraft in Wind Tunnel–Based Virtual Flight Testing

Journal of Aerospace Engineering
2023-05 | Journal article
Contributors: Shang Tai; Lixin Wang; Yanling Wang; Chen Bu; Ting Yue; Hailiang Liu
Source: check_circle
Crossref

Identification of Lateral-Directional Aerodynamic Parameters for Aircraft Based on a Wind Tunnel Virtual Flight Test

Aerospace
2023-04 | Journal article | Author
Contributors: Shang Tai; Lixin Wang; Yanling Wang; Shiguang Lu; Chen Bu; Ting Yue
Source: check_circle
Multidisciplinary Digital Publishing Institute
grade
Preferred source (of 2)‎

Similarity relations of PID flight control parameters of scaled-model and full-size aircraft

IEEE Transactions on Aerospace and Electronic Systems
2022 | Journal article
Part of ISSN: 0018-9251
Part of ISSN: 1557-9603
Part of ISSN: 2371-9877
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Longitudinal Aerodynamic Parameter Identification for Blended-Wing-Body Aircraft Based on a Wind Tunnel Virtual Flight Test

Aerospace
2022-11 | Journal article | Author
Contributors: Lixin Wang; Shang Tai; Ting Yue; Hailiang Liu; Yanling Wang; Chen Bu
Source: check_circle
Multidisciplinary Digital Publishing Institute
grade
Preferred source (of 2)‎

Wing-in-ground craft longitudinal modeling and simulation based on a moving wavy ground test

Aerospace Science and Technology
2022-07 | Journal article
Part of ISSN: 1270-9638
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Stability characteristics and airworthiness requirements of blended wing body aircraft with podded engines

Chinese Journal of Aeronautics
2022-06 | Journal article
Part of ISSN: 1000-9361
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

ESO-based nonlinear flying boom attitude control with the handling qualities requirement

Aerospace Science and Technology
2022-01 | Journal article
Part of ISSN: 1270-9638
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Envelope protection reconfiguration for iced aircraft

2021 12th International Conference on Mechanical and Aerospace Engineering, ICMAE 2021
2021 | Conference paper
Source: Self-asserted source
Lixin Wang

Influence of control surface damage on flying qualities of inter-axis motion coupling [舵面破损对飞机轴间运动耦合飞行品质的影响]

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
2021 | Journal article
Source: Self-asserted source
Lixin Wang

Prediction of longitudinal Category Ⅰ PIO of full-size aircraft based on scaled model [基于缩比模型的全尺寸飞机纵向Ⅰ类PIO预测]

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2021 | Journal article
Source: Self-asserted source
Lixin Wang

PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY

32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
2021 | Conference paper
URI:

https://www.scopus.com/inward/record.uri?eid=2-s2.0-85124492449&partnerID=40&md5=ebda00f291b42c0acdbe20c669e1c23a

Source: Self-asserted source
Lixin Wang

Simulation and evaluation method of aircraft response characteristics under wind disturbance [飞机风扰响应特性的模拟与评定方法]

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2021 | Journal article
Source: Self-asserted source
Lixin Wang

Pilot multi-axis control behavior modeling of receivers in probe-and-drogue aerial refueling

Science China Technological Sciences
2021-11-25 | Journal article
Part of ISSN: 1674-7321
Part of ISSN: 1869-1900
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Aircraft Configuration Parameter Boundaries Based on Closed-Loop Flying Qualities Requirements

Aerospace
2021-11-24 | Journal article
Part of ISSN: 2226-4310
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Method of predicting nonlinear pilot-induced oscillations due to flight control degradation based on digital virtual flight

Aerospace Science and Technology
2021-09 | Journal article
Part of ISSN: 1270-9638
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Test Data Processing of Fly-by-Wire Civil Aircraft in Low-Speed Wind Tunnel Virtual Flight

2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE)
2021-07-16 | Conference paper
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Longitudinal Flying Qualities Evaluation Method for Receiver in Probe and Drogue Aerial Refueling

ICMAE 2020 - 2020 11th International Conference on Mechanical and Aerospace Engineering
2020 | Conference paper
Source: Self-asserted source
Lixin Wang

Research on multi-task command allocation method for flying wing aircraft

IOP Conference Series: Materials Science and Engineering
2020 | Conference paper
Source: Self-asserted source
Lixin Wang

Step-by-Step Longitudinal Aerodynamic Parameter Estimation Method for Fly-by-Wire Aircraft

ICMAE 2020 - 2020 11th International Conference on Mechanical and Aerospace Engineering
2020 | Conference paper
Source: Self-asserted source
Lixin Wang

Water takeoff performance calculation method for amphibious aircraft based on digital virtual flight

Chinese Journal of Aeronautics
2020-12 | Journal article
Part of ISSN: 1000-9361
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Three-axis coupled flight control law design for flying wing aircraft using eigenstructure assignment method

Chinese Journal of Aeronautics
2020-10 | Journal article
Part of ISSN: 1000-9361
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Influence of unmanned combat aerial vehicle agility on short-range aerial combat effectiveness

Aerospace Science and Technology
2020-01 | Journal article
Part of ISSN: 1270-9638
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

An application of continuous deep reinforcement learning approach to pursuit-evasion differential game

Proceedings of 2019 IEEE 3rd Information Technology, Networking, Electronic and Automation Control Conference, ITNEC 2019
2019 | Conference paper
Source: Self-asserted source
Lixin Wang

Bank angle protection methods for a wing-in-ground craft

2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
2019 | Conference paper
Source: Self-asserted source
Lixin Wang

Control Allocation Approach Study for BWB Aircraft

Lecture Notes in Electrical Engineering
2019 | Book chapter
Part of ISBN: 9789811333040
Part of ISBN: 9789811333057
Part of ISSN: 1876-1100
Part of ISSN: 1876-1119
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Parameter suitability envelope for safety bolter of a carrier-based aircraft [舰载机安全逃逸复飞的参数适配包线]

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2019 | Journal article
Source: Self-asserted source
Lixin Wang

Pilot-induced oscillation analysis for receiver in flying-boom aerial refueling via mission-oriented evaluation

2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
2019 | Conference paper
Source: Self-asserted source
Lixin Wang

Similarity for simulating automatic carrier landing process of full-scale aircraft with scaled-model [缩比模型模拟全尺寸飞机自动着舰的相似关系]

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
2019 | Journal article
Source: Self-asserted source
Lixin Wang

A fuzzy deterministic policy gradient algorithm for pursuit-evasion differential games

Neurocomputing
2019-10 | Journal article
Part of ISSN: 0925-2312
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Closed-loop motion characteristic requirements of receiver aircraft for probe and drogue aerial refueling

Aerospace Science and Technology
2019-10 | Journal article
Part of ISSN: 1270-9638
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Flying qualities evaluation criteria design for scaled-model aircraft based on similarity theory

Aerospace Science and Technology
2019-07 | Journal article
Part of ISSN: 1270-9638
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Suggested closed-loop response characteristics for tanker in aerial refueling via mission-oriented evaluation

Science China Technological Sciences
2019-03 | Journal article
Part of ISSN: 1674-7321
Part of ISSN: 1869-1900
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 3)‎

Sliding mode control design for oblique wing aircraft in wing skewing process

Chinese Journal of Aeronautics
2019-02 | Journal article
Part of ISSN: 1000-9361
Source: Self-asserted source
Lixin Wang
grade
Preferred source (of 2)‎

Effect of asymmetric factors on carrier-based aircraft catapult launch safety

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2018 | Journal article
Source: Self-asserted source
Lixin Wang

Evaluation of directional ground stability and control characteristics in crosswind landing for civil airplane based on digital virtual flight

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2018 | Journal article
Source: Self-asserted source
Lixin Wang

Handling qualities research of flying boom for air-to-air refuelingbased on mission-oriented method [基于任务的硬式加油伸缩管操纵品质研究]

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
2018 | Journal article
Source: Self-asserted source
Lixin Wang

Influence of aerodynamic parameters on short-period mode characteristics of closed-loop aircraft

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2018 | Journal article
Source: Self-asserted source
Lixin Wang

Low-order equivalent matching methods for aircraft with flying wings

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2018 | Journal article
Source: Self-asserted source
Lixin Wang

Adjustment method of automatic carrier landing system design criterion for scaled model aircraft

Chinese Control Conference, CCC
2017 | Conference paper
Source: Self-asserted source
Lixin Wang

An nonlinear feedback control for radial constrained force of flying boom after contact with receiver

2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
2017 | Conference paper
Source: Self-asserted source
Lixin Wang

Analysis of design principle adaptability to automatic carrier landing system of light plane

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2017 | Journal article
Source: Self-asserted source
Lixin Wang

Assessment of go-around climb gradient for civil aircraft based on digital virtual flight

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2017 | Journal article
Source: Self-asserted source
Lixin Wang

Crosswind take-off and landing characteristics of flying wings

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
2017 | Journal article
Source: Self-asserted source
Lixin Wang

Design of flying boom controller before and after docking

CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
2017 | Conference paper
Source: Self-asserted source
Lixin Wang

Dynamic characteristics analysis for oblique wing aircraft

CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
2017 | Conference paper
Source: Self-asserted source
Lixin Wang

Flight dynamic modeling and control for a telescopic wing morphing aircraft via asymmetric wing morphing

Aerospace Science and Technology
2017 | Journal article
Source: Self-asserted source
Lixin Wang
Items per page:
Page 1 of 3