A Heading and Flight-Path Angle Control of Aircraft Based on Required Acceleration Vector-Reference-Cited by-同舟云学术

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A Heading and Flight-Path Angle Control of Aircraft Based on Required Acceleration Vector

Published:2004 Issue:605 Volume:52 Page:265-271
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Yoshitani Naoharu

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/52/605/52_605_265/_pdf

Reference6 articles.

1. Given flight trajectory controller for aircraft.

2. 2) 馬場順昭,高野博行,佐野正樹:航空機の目標経路への誘導と制御,第12回誘導制御シンポジウム,1995, pp. 147–154.

3. Four-dimensional guidance of atmospheric vehicles

4. 6) G. ジェニングズ(伊里正夫.伊里由美訳): 幾何再入門,岩波書店,東京,1996.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Lateral Guidance Control of UAV Using Feedback Error Learning;AIAA Infotech@Aerospace 2007 Conference and Exhibit;2007-05-07

2. A Flight-Path Control of Aircraft Based on Required Acceleration Vector;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007

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