Energy-Optimal Waypoint-Following Guidance Law Considering Autopilot Dynamics

Shaoming He; Chang Hun Lee; Hyo Sang Shin; Antonios Tsourdos

doi:10.1007/978-3-030-47348-8_9

Energy-Optimal Waypoint-Following Guidance Law Considering Autopilot Dynamics

Shaoming He^*, Chang Hun Lee, Hyo Sang Shin, Antonios Tsourdos

^*此作品的通讯作者

宇航学院

科研成果: 书/报告/会议事项章节 › 章节 › 同行评审

摘要

This chapter addresses the problem of energy-optimal waypoint-following guidance for a UAV with the consideration of a general autopilot dynamics model. The proposed guidance law is derived as a solution of a linear quadratic optimal control problem in conjunction with a linearized kinematics model. The algorithm developed integrates path planning and following into a single step and is able to be applied to a general waypoint-following mission. Theoretical analysis reveals that previously suggested optimal point-to-point guidance laws are special cases of the proposed approach. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.

源语言	英语
主期刊名	Springer Aerospace Technology
出版商	Springer Nature
页	175-198
页数	24
DOI	https://doi.org/10.1007/978-3-030-47348-8_9
出版状态	已出版 - 2020

出版系列

姓名	Springer Aerospace Technology
ISSN（印刷版）	1869-1730
ISSN（电子版）	1869-1749

访问文件

10.1007/978-3-030-47348-8_9

其它文件与链接

链接到 Scopus 的出版物

引用此

He, S., Lee, C. H., Shin, H. S., & Tsourdos, A. (2020). Energy-Optimal Waypoint-Following Guidance Law Considering Autopilot Dynamics. 在 Springer Aerospace Technology (页码 175-198). (Springer Aerospace Technology). Springer Nature. https://doi.org/10.1007/978-3-030-47348-8_9

@inbook{add604160a3c401d9509146f99367914,

title = "Energy-Optimal Waypoint-Following Guidance Law Considering Autopilot Dynamics",

abstract = "This chapter addresses the problem of energy-optimal waypoint-following guidance for a UAV with the consideration of a general autopilot dynamics model. The proposed guidance law is derived as a solution of a linear quadratic optimal control problem in conjunction with a linearized kinematics model. The algorithm developed integrates path planning and following into a single step and is able to be applied to a general waypoint-following mission. Theoretical analysis reveals that previously suggested optimal point-to-point guidance laws are special cases of the proposed approach. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.",

author = "Shaoming He and Lee, {Chang Hun} and Shin, {Hyo Sang} and Antonios Tsourdos",

note = "Publisher Copyright: {\textcopyright} 2020, The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerland AG.",

year = "2020",

doi = "10.1007/978-3-030-47348-8_9",

language = "English",

series = "Springer Aerospace Technology",

publisher = "Springer Nature",

pages = "175--198",

booktitle = "Springer Aerospace Technology",

address = "Switzerland",

}

TY - CHAP

T1 - Energy-Optimal Waypoint-Following Guidance Law Considering Autopilot Dynamics

AU - He, Shaoming

AU - Lee, Chang Hun

AU - Shin, Hyo Sang

AU - Tsourdos, Antonios

PY - 2020

Y1 - 2020

N2 - This chapter addresses the problem of energy-optimal waypoint-following guidance for a UAV with the consideration of a general autopilot dynamics model. The proposed guidance law is derived as a solution of a linear quadratic optimal control problem in conjunction with a linearized kinematics model. The algorithm developed integrates path planning and following into a single step and is able to be applied to a general waypoint-following mission. Theoretical analysis reveals that previously suggested optimal point-to-point guidance laws are special cases of the proposed approach. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.

AB - This chapter addresses the problem of energy-optimal waypoint-following guidance for a UAV with the consideration of a general autopilot dynamics model. The proposed guidance law is derived as a solution of a linear quadratic optimal control problem in conjunction with a linearized kinematics model. The algorithm developed integrates path planning and following into a single step and is able to be applied to a general waypoint-following mission. Theoretical analysis reveals that previously suggested optimal point-to-point guidance laws are special cases of the proposed approach. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.

UR - http://www.scopus.com/inward/record.url?scp=85101590788&partnerID=8YFLogxK

U2 - 10.1007/978-3-030-47348-8_9

DO - 10.1007/978-3-030-47348-8_9

M3 - Chapter

AN - SCOPUS:85101590788

T3 - Springer Aerospace Technology

SP - 175

EP - 198

BT - Springer Aerospace Technology

PB - Springer Nature

ER -

Energy-Optimal Waypoint-Following Guidance Law Considering Autopilot Dynamics

摘要

出版系列

访问文件

其它文件与链接

指纹

引用此