云南高校图书馆联盟文献共享服务平台- OPTIMAL

OPTIMAL_CONTROL: 作品数：613被引量：1054H指数：13; 导出分析报告; 相关作者：蔡其发黄思训李永进孙健国刘会坡更多>>; 相关机构：南京航空航天大学东南大学北京理工大学解放军理工大学更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金国家重点基础研究发展计划国家教育部博士点基金中国博士后科学基金更多>>

Cooperative guidance law with maneuverability awareness:A decentralized solution被引量：1: 《Chinese Journal of Aeronautics》2024年第7期450-457,共8页Shuyang XU Xun SONG Chaoyong LI; supported by the NSFC 62088101 Autonomous Intelligent Unmanned Systems,China;by the Zhejiang Provincial Natural Science Foundation of China(No.LR20F030003).; In this paper,we propose a cooperative guidance law aimed to achieve coordinated impact angles with limited observation on target information.The primary challenge lies in establishing an appropriate communication gra...; 关键词：Cooperative guidance Target maneuver estimation Distributed estimation CONSENSUS Optimal control

Neighboring optimal guidance using higher-order dynamics approximation with application to orbital injection problem: 《Chinese Journal of Aeronautics》2024年第5期426-440,共15页Xinglun CHEN Ran ZHANG Huifeng LI; This study was co-supported by the National Natural Science Foundation of China(No.62103014).; Neighboring optimal guidance,a method to obtain a suboptimal guidance law by approximately solving the first-order necessary conditions based on a nominal trajectory,is widely used in the aerospace field due to its hi...; 关键词：Optimal control Neighboring optimal guidance Launch vehicles Orbital injection Higher-order approximation

Convex optimization of asteroid landing trajectories driven by solar radiation pressure被引量：3: 《Chinese Journal of Aeronautics》2022年第12期200-211,共12页Chuanjun DONG Hongwei YANG Shuang LI Bo LI; supported by the National Natural Science Foundation of China(No.12102177);the Natural Science Foundation of Jiangsu Province,China(No.BK20180410);the Young Elite Scientists Sponsorship Program by CAST,China(No.2018QNRC001);the Open Project Program of Tianjin Key Laboratory of Microgravity and Hypogravity Environment Simulation Technology,China(No.WDZL2020-07);the Foundation of Graduate Innovation Center at NUAA,China(No.kfjj20201503).; High-area/mass ratio landers driven by Solar Radiation Pressure(SRP)have potential applications for future asteroid landing missions.This paper develops a new convex optimization-based method for planning trajectories...; 关键词：ASTEROIDS Convex optimization Optimal control Soft landing Solar radiation pressure Trajectory optimization

Smooth free-cycle dynamic soaring in unspecified shear wind via quadratic programming被引量：4: 《Chinese Journal of Aeronautics》2022年第7期19-29,共11页Haichao HONG Benedikt GRüTER Patrick PIPREK Florian HOLZAPFEL; supported in part by the TUM University Foundation Fellowship;in part by the German Federal Ministry for Economic Affairs and Energy(BMWi)within the Federal Aeronautical Research Program LuFo VI-1through Project“RAUDY”(No.20E1910B)。; Harvesting wind energy is promising for extending long-endurance flights,which can be greatly facilitated by a flight technique called dynamic soaring.The presented study is concerned with generating model-based traje...; 关键词：Dynamic soaring Optimal control Quadratic programming Trajectory generation Trigonometric series

Optimal trajectory design accounting for the stabilization of linear time-varying error dynamics: 《Chinese Journal of Aeronautics》2022年第7期55-66,共12页Patrick PIPREK Haichao HONG Florian HOLZAPFEL; supported in part by the TUM University Foundation Fellowship;in part by the German Federal Ministry for Economic Affairs and Energy(BMWi)within the Federal Aeronautical Research Program LuFo V-3 through Project“HOTRUN”(No.20E1720A)。; This study is dedicated to the development of a direct optimal control-based algorithm for trajectory optimization problems that accounts for the closed-loop stability of the trajectory tracking error dynamics already...; 关键词：LTV error dynamics LTV stability Optimal control-based LTV stabilization Path-following error controller Trajectory generation Trajectory optimization

Sub-optimal fixed-finite-horizon spacecraft configuration control on SE(3)被引量：1: 《Chinese Journal of Aeronautics》2022年第6期250-261,共12页Yulin WANG Wei SHANG Haichao HONG; the support of the TUM University Foundation Fellowship。; For achieving the desired configuration of spacecraft at the desired fixed time,a suboptimal fixed-finite-horizon configuration control method on the Lie group SE(3)is developed based on the Model Predictive Static Pr...; 关键词：Configuration control Lie groups Model Predictive Static Programming Optimal control Spacecraft control

Design method of optimal control schedule for the adaptive cycle engine steady-state performance被引量：5: 《Chinese Journal of Aeronautics》2022年第4期148-164,共17页Yihao XU Hailong TANG Min CHEN; funded by National Nature Science Foundation of China(Nos.51776010 and 91860205);supported by the Academic Excellence Foundation of BUAA for PhD Students,China。; The alternative working modes and flexible working states are the outstanding features of an adaptive cycle engine, with a proper control schedule design being the only way to exploit the performance of such an engine...; 关键词：Adaptive cycle engine Control schedule design Hybrid optimization method Mode transition Performance optimization

Optimal predictive sliding-mode guidance law for intercepting near-space hypersonic maneuvering target被引量：5: 《Chinese Journal of Aeronautics》2022年第4期320-331,共12页Bolun ZHANG Di ZHOU; supported by the National Natural Science Foundation of China(No.61773142)。; The design of optimal guidance law for intercepting a near-space hypersonic maneuvering target with bounded inputs is considered. Firstly, a maneuvering model for near-space hypersonic aircraft is given. Then, the air...; 关键词：Adaptive sliding-mode control Near-space hypersonic aircraft Neural networks Optimal control Predictive guidance law

Discrete time multiple spacecraft formation flying attitude optimal control in presence of relative state constraints被引量：4: 《Chinese Journal of Aeronautics》2021年第4期293-305,共13页Hossein MORADI PARI Hossein BOLANDI; This paper addresses the challenge of synchronized multiple spacecraft attitude reorientation in presence of pointing and boundary constraints with limited inter-spacecraft communication link.Relative attitude pointin...; 关键词：DECENTRALIZED Discrete time Formation flying Optimal control SPACECRAFT Virtual structure approach

Modified robust optimal adaptive control for flight environment simulation system with heat transfer uncertainty被引量：3: 《Chinese Journal of Aeronautics》2021年第2期420-431,共12页Meiyin ZHU Xi WANG Xitong PEI Song ZHANG Zhihong DAN Nannan GU Shubo YANG Keqiang MIAO Huairong CHEN Jiashuai LIU; funded by China Scholarship Council (CSC)and National Science and Technology Major Project,China(No. 2017-V-0015-0067)。; To solve the rapid transient control problem of Flight Environment Simulation System(FESS) of Altitude Ground Test Facilities(AGTF) with large heat transfer uncertainty and disturbance, a new adaptive control structur...; 关键词：Altitude ground test facilities Flight environment simulation system Heat transfer Model reference adaptive control Optimal control modification UNCERTAINTY

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