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IR-UWB Radar 기반 무인기 안전착륙을 위한 고도 측정에 관한 연구

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Alternative Title
A Study on the Altitude Measurement for the Safe Landing of IR-UWB Radar-based UAV
Abstract
It is expected that the following future will face various use cases of UAV (Unmanned Aerial Vehicle), including our daily life, industrial fields and military purposes. Further, it is regarded that UAV should be utilized in various conditions such as the increase in takeoff weight. However, these conditions may cause a lot of mechanical problems including the malfunction of state estimation sensors, the increase in impulse force and securing flight time, which is a disadvantage for takeoff and landing.
In this context, this paper have examined how to advance these conditional problems, and it suggests the way of precision altitude measurement in the unit of cm with cross-correlation signal processing technique and band pass filter, using the IR-UWB Radar which can be used for strong and precise state estimation for environmental factors and consumes lower electric power. In addition, this paper utilized the mission planner which can monitor the state of UAV in order to check out takeoff and landing characteristics of UAV, based on altitude data, and it monitored the throttle for each state of UAV and servomotor output data in real time. In addition, it repeatedly experimented with takeoff and landing of UAV to get the throttle and the output data. It also utilized the data and controlled the UAV of 6kg and conducted a landing test at the first altitude of 50cm and the second altitude of 10cm to confirm the stability of UAV. Likewise, In case of the currently developing UAV, it used ABAQUS Explicit Non-Linear and simulated its landing situations at the altitude of 10 cm to confirm its stability.
Author(s)
임재준
Issued Date
2018
Awarded Date
2018. 8
Type
Dissertation
Publisher
부경대학교
URI
https://repository.pknu.ac.kr:8443/handle/2021.oak/14551
http://pknu.dcollection.net/common/orgView/200000115667
Affiliation
부경대학교 대학원
Department
대학원 제어계측공학과
Advisor
변기식
Table Of Contents
목 차ⅰ
그림 차례 ⅲ
표 차례 ⅴ
Abstract ⅵ

제 1 장 서론 1

제 2 장 무인기 시스템 3
2.1 무인기의 상태추정 3
2.2 전파고도계의 고도 측정 원리 4
2.3 무인기 운영환경과 착륙문제점 5
2.4 무인기 착륙장치의 안정성 검증 7

제 3 장 UWB 이론 10
3.1 UWB 기술개요 10
3.2 고도측정 센서 성능평가 11
3.3 IR-UWB Radar를 이용한 고도 측정 12
3.4 레이더의 종류 14

제 4장 IR-UWB Radar 신호처리 16
4.1 IR-UWB Radar 수신 신호 처리 절차 16
4.2 FIR Bandpass Filter 설계 17
4.3 Cross-Correlation기법 20

제 5장 IR-UWB Radar 기반 고도측정 실험 22
5.1 IR-UWB Radar Module 22
5.2 실험 환경 구성 24
5.3 IR-UWB Radar를 이용한 신호처리 26

제 6 장 IR-UWB Radar 고도기반 착륙 실험 33
제 7 장 결론 42
참고문헌 44
Degree
Master
Appears in Collections:
대학원 > 제어계측공학과
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