Automatic following for uavs using dynamic inversion

Author

Enomoto, Keisuke ; Yamasaki, Takeshi ; Takano, Hiroyuki ; Baba, Yoriaki

Author_Institution

Nat. Defense Acad. of Japan, Yokosuka

fYear

2007

fDate

17-20 Sept. 2007

Firstpage

2240

Lastpage

2246

Abstract

This paper introduces guidance and control system design for automatic chase UAVs. The system may contribute UAV´s multi-capabilities to conduct a variety of missions. The automatic chase guidance and control system is introduced with the pure pursuit guidance law combined with relative velocity error correction using variable gains, and a dynamic inversion technique in order to correct and generate the guidance forces.

Keywords

aircraft control; control system synthesis; mobile robots; remotely operated vehicles; velocity control; automatic chase UAV; control system; dynamic inversion; guidance system; pursuit guidance law; variable gains; velocity error correction; Automatic control; Automatic generation control; Control systems; Error correction; Force control; Gain; Velocity control; UAV; automatic; dynamic inversion; pure pursuit guidance;

fLanguage

English

Publisher

ieee

Conference_Titel

SICE, 2007 Annual Conference

Conference_Location

Takamatsu

Print_ISBN

978-4-907764-27-2

Electronic_ISBN

978-4-907764-27-2

Type

conf

DOI

10.1109/SICE.2007.4421361

Filename

4421361

Link To Document

https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2642871