于存贵 , 李志刚 . 火箭发射系统分析 [M ] . 北京 : 国防工业出版社 , 2012 .

YU C G , LI Z G . Rocket launch system analysis [M ] . Beijing : National Defense Industry Press , 2012 . (in Chinese)

张琳 , 龚喜盈 , 张晓辉 . 火箭助推零长发射建模仿真研究 [J ] . 火力与指挥控制 , 2019 , 44 ( 8 ): 150 - 154 .

ZHANG L , GONG X Y , ZHANG X H . Modeling and simulation research on rocket boosted zero-length launching [J ] . Fire Control & Command Control , 2019 , 44 ( 8 ): 150 - 154 . (in Chinese)

LI D W , WANG H L , GAI W D . Application of a feedforward controller with a disturbance observer for UAV during missile launch [C ] // Proceedings of the 2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce. Dengfeng, China:IEEE , 2011 .

LIU R , XIAO Y F , ZHANG H . The algorithm research based on optimal quadratic of launch control law access time of folding wing UAV [C ] // Proceedings of 2018 International Conference on Computer, Communications and Mechatronics Engineering. Lancaster, PA , US : DEStech Publications , 2018 : 603 - 611 .

姚琳 , 王晓东 . 无人机助推起飞过程影响因素敏感度分析 [J ] . 兵器装备工程学报 , 2020 , 41 ( 10 ): 81 - 85 .

YAO L , WANG X D . Analysis of sensitive factors and dynamic performance on launching process of a UAV [J ] . Journal of Ordnance Equipment Engineering , 2020 , 41 ( 10 ): 81 - 85 . (in Chinese)

刘付平 , 郑耀 , 谢芳芳 , 等 . 助推火箭安装偏差对小型无人机发射安全的影响 [J ] . 哈尔滨工程大学学报 , 2018 , 39 ( 8 ): 1343 - 1348 .

LIU F P , ZHENG Y , XIE F F , et al . Effects of a booster rocket installation deviation on the launch safety of a small unmanned aerial vehicle [J ] . Journal of Harbin Engineering University , 2018 , 39 ( 8 ): 1343 - 1348 . (in Chinese)

陶于金 . 小型固定翼无人机零长发射参数安全边界研究 [J ] . 海军航空工程学院学报 , 2017 , 32 ( 5 ): 447 - 451 ,468.

TAO Y J . Research on zero-length launch parameters safety boundary of small fixed-wing UAVs [J ] . Journal of Naval Aeronautical and Astronautical University , 2017 , 32 ( 5 ): 447 - 451 ,468. (in Chinese)

王晓东 , 夏杨 , 涂金岽 . 一种无人机火箭助推器脱落导向结构: CN211281514U [P ] . 2020 -08-18.

WANG X D , XIA Y , TU J D . The invention relates to an UAV rocket booster shedding guide structure: CN211281514U [P ] . 2020 -08-18. (in Chinese)

陈刚 . 无人机单(双)火箭助推发射安全性对比分析 [J ] . 四川兵工学报 , 2021 , 42 ( 8 ): 27 - 32 .

CHEN G . Comparative analysis of UAV launching safety by using single or double solid-rocket booster [J ] . Journal of Sichuan Ordnance , 2021 , 42 ( 8 ): 27 - 32 . (in Chinese)

YIN J , ZHANG B , ZHAO L X , et al . Simulation and analysis of short rail launch for UAV with rocket booster [C ] // Proceedings of the 2020 3rd International Conference on Unmanned Systems. Harbin, China:IEEE , 2020 .

XU J H , WANG L J , LIU Y , et al . Finite-time prescribed performance optimal attitude control for quadrotor UAV [J ] . Applied Mathematical Modelling , 2023 , 120 ( 1 ): 752 - 768 . DOI: 10.1016/j.apm.2023.03.030 http://doi.org/10.1016/j.apm.2023.03.030 https://linkinghub.elsevier.com/retrieve/pii/S0307904X23001294 https://linkinghub.elsevier.com/retrieve/pii/S0307904X23001294

乐文超 , 朱晓 , 宁月敏 , 等 . 基于fmincon的扭杆悬架弹簧优化设计 [J ] . 上海汽车 , 2018 ( 6 ): 13 - 18 .

LE W C , ZHU X , NING Y M , et al . Optimal design of the torsion bar spring based on fmincon [J ] . Shanghai Auto , 2018 ( 6 ): 13 - 18 . (in Chinese)

YAP Y L , TOH W , GIAM A , et al . Topology optimization and 3D printing of micro-drone: Numerical design with experimental testing [J ] . International Journal of Mechanical Sciences , 2023 , 237 ( 1 ): 107771 . DOI: 10.1016/j.ijmecsci.2022.107771 http://doi.org/10.1016/j.ijmecsci.2022.107771 https://linkinghub.elsevier.com/retrieve/pii/S0020740322006518 https://linkinghub.elsevier.com/retrieve/pii/S0020740322006518

DA SILVA R A C , DA FONSECA N L S . Location of fog nodes mounted on fixed-wing UAVs [J ] . Vehicular Communications , 2023 , 41 ( 1 ): 100600 . DOI: 10.1016/j.vehcom.2023.100600 http://doi.org/10.1016/j.vehcom.2023.100600 https://linkinghub.elsevier.com/retrieve/pii/S221420962300030X https://linkinghub.elsevier.com/retrieve/pii/S221420962300030X

ZHOU W , MA P Y , WEI B B , et al . Experimental study on aerodynamic characteristics of fixed-wing UAV air docking [J ] . Aerospace Science and Technology , 2023 , 137 ( 1 ): 108257 . DOI: 10.1016/j.ast.2023.108257 http://doi.org/10.1016/j.ast.2023.108257 https://linkinghub.elsevier.com/retrieve/pii/S1270963823001542 https://linkinghub.elsevier.com/retrieve/pii/S1270963823001542

王盼 , 吴昊 , 梁宇 , 等 . 轻型无人机起落架设计与强度分析 [J ] . 兵工学报 , 2022 , 43 ( 增刊1 ): 140 - 145 .

WANG P , WU H , LIANG Y , et al . Design and strength analysis of light UAV landing gear [J ] . Acta Armamentarii , 2022 , 43 ( S1 ): 140 - 145 . (in Chinese) DOI: 10.12382/bgxb.2022.A023 http://doi.org/10.12382/bgxb.2022.A023 A landing gear for a specific light UAV is designed and analyzed to make up for the lack of research on the landing gear or flight-assisting system of light UAVs. According to the actual application requirements，a design scheme of the landing gear structure and electrical system of a light UAV was proposed. Based on the weight of UAV，Ansys simulation software is used to establish a finite element calculation model，and the strength of landing gear structure was analyzed and simulated. The results of structural strength analysis show that the maximum deformation of landing gear is 0.6 mm，which meets the design requirements.The light UAV landing gear designed in this paper has the advantages of simple structure，light weight and high reliability，which provides a solution for related research and engineering applications.

HEIDARI H , SASKA M . Collision-free trajectory planning of multi-rotor UAVs in a wind condition based on modified potential field [J ] . Mechanism and Machine Theory , 2021 , 156 ( 1 ): 104140 . DOI: 10.1016/j.mechmachtheory.2020.104140 http://doi.org/10.1016/j.mechmachtheory.2020.104140 https://linkinghub.elsevier.com/retrieve/pii/S0094114X20303578 https://linkinghub.elsevier.com/retrieve/pii/S0094114X20303578

PARK S H , LEE S , LM B , et al . Improvement of a multi-rotor UAV flight response simulation influenced by gust [J ] . Aerospace Science and Technology , 2023 , 134 ( 1 ): 108156 . DOI: 10.1016/j.ast.2023.108156 http://doi.org/10.1016/j.ast.2023.108156 https://linkinghub.elsevier.com/retrieve/pii/S1270963823000536 https://linkinghub.elsevier.com/retrieve/pii/S1270963823000536

CHU L L , GU F , DU X T , et al . Aerodynamic configuration and control optimization for a novel horizontal-rope shipborne recovery fixed-wing UAV system [J ] . Aerospace Science and Technology , 2023 , 137 ( 1 ): 108253 . DOI: 10.1016/j.ast.2023.108253 http://doi.org/10.1016/j.ast.2023.108253 https://linkinghub.elsevier.com/retrieve/pii/S1270963823001505 https://linkinghub.elsevier.com/retrieve/pii/S1270963823001505

CONG K , MA D L , ZHANG L , et al . Design and analysis of passive variable-pitch propeller for VTOL UAVs [J ] . Aerospace Science and Technology , 2023 , 132 ( 1 ): 108063 . DOI: 10.1016/j.ast.2022.108063 http://doi.org/10.1016/j.ast.2022.108063 https://linkinghub.elsevier.com/retrieve/pii/S1270963822007374 https://linkinghub.elsevier.com/retrieve/pii/S1270963822007374