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检索条件"主题词=Guidance and Navigational Algorithms"
27 条 记 录,以下是1-10 订阅
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Impact Time Control guidance Using Output Trajectory Shaping Method
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JOURNAL OF guidance CONTROL AND DYNAMICS 2025年 第4期48卷 961-967页
作者: Lee, Suwon Kim, Mingu Tekin, Raziye Kookmin Univ Dept Future Mobil 77 Jeongneung Ro Seoul 02707 South Korea Hansung Univ Div Mech & Elect Engn Seoul 02876 South Korea Roketsan Missiles Inc Tactical Missile Syst TR-06780 Ankara Turkiye
来源: 评论
Lyapunov guidance Vector Field-Based Waypoint Following by Unmanned Aerial Vehicles
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JOURNAL OF guidance CONTROL AND DYNAMICS 2025年 第1期48卷 192-202页
作者: Harinarayana, Tammineni Krishnan, Siva Vignesh Hota, Sikha Indian Inst Technol Dept Aerosp Engn Kharagpur 721302 India
来源: 评论
Line-of-Sight-Constrained Multicopter Interceptability
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JOURNAL OF guidance CONTROL AND DYNAMICS 2025年 第4期48卷 951-960页
作者: Yang, Kun Bai, Chenggang Quan, Quan Beihang Univ Sch Automat Sci & Elect Engn Beijing 100191 Peoples R China
来源: 评论
Robust Launch Vehicle Trajectory Optimization with Stage Impact and Heat Flux Constraints
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JOURNAL OF SPACECRAFT AND ROCKETS 2023年 第4期60卷 1268-1283页
作者: Swaminathan, Shriram Rajeev, U. P. Ghose, Debasish Indian Space Res Org Vikram Sarabhai Space Ctr Guidance Design Div Veli Perumathura Rd Thiruvananthapuram 695022 Kerala India Indian Space Res Org Vikram Sarabhai Space Ctr Control & Guidance Design Grp Veli Perumathura Rd Thiruvananthapuram 695022 Kerala India Indian Inst Sci Aerosp Engn Dept CV Raman Rd Bengaluru 560012 Karnataka India
A fast trajectory optimization/guidance algorithm in the presence of path constraints for a multistage launch vehicle is presented in this work. The optimization problem is to maximize the payload to be injected into ... 详细信息
来源: 评论
Abort guidance During Lunar Powered Descent
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JOURNAL OF guidance CONTROL AND DYNAMICS 2024年 第3期47卷 394-406页
作者: Sandoval, Sergio A. Lu, Ping Hwang, John T. San Diego State Univ San Diego CA 92182 USA NASA Johnson Space Ctr Houston TX 77058 USA San Diego State Univ Dept Aerosp Engn San Diego CA 92182 USA Univ Calif San Diego Dept Mech & Aerosp Engn San Diego CA 92093 USA
During powered descent of a crewed lunar landing mission, the ability to abort and ascend into a clear pericynthion orbit is critical in case any contingency renders the landing infeasible or excessively risky. In suc... 详细信息
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Energy-Efficient Ring Formation Control with Constrained Inputs
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JOURNAL OF guidance CONTROL AND DYNAMICS 2023年 第7期46卷 1397-1407页
作者: Ranjan, Praveen Kumar Sinha, Abhinav Cao, Yongcan Tran, Dzung Casbeer, David Weintraub, Isaac Univ Texas San Antonio Unmanned Syst Lab Dept Elect & Comp Engn San Antonio TX 78249 USA US Air Force Res Lab Control Sci Ctr Wright Patterson AFB OH 45433 USA
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Urban Air Mobility guidance with Panel Method: Experimental Evaluation Under Wind Disturbances
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JOURNAL OF guidance CONTROL AND DYNAMICS 2024年 第6期47卷 1080-1096页
作者: Bilgin, Zeynep Yavrucuk, Ilkay Bronz, Murat Tech Univ Munich Inst Rotorcraft & Vert Flight TUM Sch Engn & Design D-85748 Garching Germany Tech Univ Munich Inst Rotorcraft & Vert Flight TUM Sch Engn & Design D-85748 Garching Germany Univ Toulouse Ecole Natl Aviat Civile ENAC Lab Dynam SystENAC F-31400 Toulouse France
In this paper, a nature-inspired guidance algorithm based on the panel method is proposed. The panel method is a numerical tool borrowed from the aerodynamics domain to calculate the potential field of a fluid flow ar... 详细信息
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Multi-Objective Robust Trajectory Design for Powered Descent and Landing
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JOURNAL OF SPACECRAFT AND ROCKETS 2024年 第6期61卷 1496-1509页
作者: Calkins, Grace E. Putnam, Zachary R. Woffinden, David C. Univ Illinois Aerosp Engn Dept 104 S Wright St Urbana IL 61801 USA NASA Johnson Space Ctr GN&C Autonomous Syst Branch Houston TX 77508 USA
A robust trajectory optimization approach for guidance algorithm gain and target vector selection for powered descent and landing is developed. A genetic algorithm is used to determine optimized guidance algorithm par... 详细信息
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Onboard Burn Targeting and guidance of NASA Human Flight Vehicles
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JOURNAL OF guidance CONTROL AND DYNAMICS 2024年 第11期47卷 2241-2258页
作者: Goodman, John L. Odyssey Space Res LLC Houston TX 77058 USA
The mission requirements of crewed space vehicles flown by NASA drove the development of new techniques for burn targeting and guidance for ascent, rendezvous, lunar landing, and deorbit. The Saturn V Iterative Guidan... 详细信息
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Time-Constrained Interception with Bounded Field of View and Input Using Barrier Lyapunov Approach
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JOURNAL OF guidance CONTROL AND DYNAMICS 2024年 第2期47卷 384-393页
作者: Singh, Swati Kumar, Shashi Ranjan Mukherjee, Dwaipayan Indian Inst Technol Intelligent Syst & Control Lab Dept Aerosp Engn Mumbai 400076 India Indian Inst Technol Dept Elect Engn Mumbai 400076 India
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