Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method

Kun Wu; Zhihao Cai; Qing Lin; Yingxun Wang

doi:10.1109/CGNCC.2014.7007507

Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method

Beihang University

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

Aiming at the problem of an emergency landing of unpowered aircraft, this paper presents the design of landing trajectory. Firstly, the effect of the shear wind for the flight path is considered. Secondly, the problem of unpowered flight's landing is modeled by the time-optimal control method. The landing trajectory is divided into four piecewise trajectories and the characteristics of each are determined by some simple equations. The deflection angle of turn is obtained by the Dubins curves method. Thirdly, the problem is solved by the hp-adaptive radau pseudospectral method. Simulation results indicate that the designed landing trajectory could guide the unpowered plane landed safely and quickly.

源语言	英语
主期刊名	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
出版商	Institute of Electrical and Electronics Engineers Inc.
页	2150-2155
页数	6
ISBN（电子版）	9781479946990
DOI	https://doi.org/10.1109/CGNCC.2014.7007507
出版状态	已出版 - 12 1月 2015
活动	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, 中国期限: 8 8月 2014 → 10 8月 2014

出版系列

姓名	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

会议

会议	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
国家/地区	中国
市	Yantai
时期	8/08/14 → 10/08/14

访问文件

10.1109/CGNCC.2014.7007507

其它文件与链接

链接到 Scopus 的出版物

引用此

Wu, K., Cai, Z., Lin, Q., & Wang, Y. (2015). Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method. 在 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 (页码 2150-2155). 文章 7007507 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2014.7007507

Wu, Kun ; Cai, Zhihao ; Lin, Qing 等. / Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method. 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. 页码 2150-2155 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014).

@inproceedings{b411b73c9e5445e7a924e2327d660b3e,

title = "Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method",

abstract = "Aiming at the problem of an emergency landing of unpowered aircraft, this paper presents the design of landing trajectory. Firstly, the effect of the shear wind for the flight path is considered. Secondly, the problem of unpowered flight's landing is modeled by the time-optimal control method. The landing trajectory is divided into four piecewise trajectories and the characteristics of each are determined by some simple equations. The deflection angle of turn is obtained by the Dubins curves method. Thirdly, the problem is solved by the hp-adaptive radau pseudospectral method. Simulation results indicate that the designed landing trajectory could guide the unpowered plane landed safely and quickly.",

author = "Kun Wu and Zhihao Cai and Qing Lin and Yingxun Wang",

note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 ; Conference date: 08-08-2014 Through 10-08-2014",

year = "2015",

month = jan,

day = "12",

doi = "10.1109/CGNCC.2014.7007507",

language = "英语",

series = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "2150--2155",

booktitle = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

address = "美国",

}

Wu, K , Cai, Z, Lin, Q & Wang, Y 2015, Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method. 在 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014., 7007507, 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Institute of Electrical and Electronics Engineers Inc., 页码 2150-2155, 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Yantai, 中国, 8/08/14. https://doi.org/10.1109/CGNCC.2014.7007507

Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method. / Wu, Kun ; Cai, Zhihao; Lin, Qing 等.
2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. 页码 2150-2155 7007507 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method

AU - Wu, Kun

AU - Cai, Zhihao

AU - Lin, Qing

AU - Wang, Yingxun

PY - 2015/1/12

Y1 - 2015/1/12

N2 - Aiming at the problem of an emergency landing of unpowered aircraft, this paper presents the design of landing trajectory. Firstly, the effect of the shear wind for the flight path is considered. Secondly, the problem of unpowered flight's landing is modeled by the time-optimal control method. The landing trajectory is divided into four piecewise trajectories and the characteristics of each are determined by some simple equations. The deflection angle of turn is obtained by the Dubins curves method. Thirdly, the problem is solved by the hp-adaptive radau pseudospectral method. Simulation results indicate that the designed landing trajectory could guide the unpowered plane landed safely and quickly.

AB - Aiming at the problem of an emergency landing of unpowered aircraft, this paper presents the design of landing trajectory. Firstly, the effect of the shear wind for the flight path is considered. Secondly, the problem of unpowered flight's landing is modeled by the time-optimal control method. The landing trajectory is divided into four piecewise trajectories and the characteristics of each are determined by some simple equations. The deflection angle of turn is obtained by the Dubins curves method. Thirdly, the problem is solved by the hp-adaptive radau pseudospectral method. Simulation results indicate that the designed landing trajectory could guide the unpowered plane landed safely and quickly.

UR - https://www.scopus.com/pages/publications/84922567616

U2 - 10.1109/CGNCC.2014.7007507

DO - 10.1109/CGNCC.2014.7007507

M3 - 会议稿件

AN - SCOPUS:84922567616

T3 - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

SP - 2150

EP - 2155

BT - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Y2 - 8 August 2014 through 10 August 2014

ER -

Wu K , Cai Z, Lin Q, Wang Y. Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method. 在 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc. 2015. 页码 2150-2155. 7007507. (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). doi: 10.1109/CGNCC.2014.7007507

Design of landing trajectory for unpowered aircraft using an hp-adaptive Radau pseudospectral method

摘要

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