Aircraft landing orbit design

DOI

10.2991/iemb-15.2015.50How to use a DOI?

Keywords

conservation of energy conservation of angular momentum of Newton's second law

Abstract

this paper focuses on The aircraft soft-landing trajectory design and control strategy of in-depth discussion and analysis of considering The aircraft landing during the motion, and the stress is different, a mathematical model, answers the questions posed by the topic. Considered actual flight situation, we established landing cabin mathematics model description The Aircraft, of movement State, according to established of model, repeatedly set angle of pitch by using Matlab , looking for meet design requirements optimal solutions, obtained optimal design points location of cross, and ordinate; in according to geometry obtained in recent months points and optimal design points of angle, according to longitude degrees calculation method, determines in recent months points, and far months points of location;When the aircraft landing elliptical orbit, it follows the conservation of energy, so the Aircraft, in recent months points and far months points of energy equal, and due to aircraft, in in recent months points and far months points of speed are and aircraft, to months heart of line vertical, is angular momentum conservation, according to gold proportions substitution, obtained has in recent months points and far months points of speed size and direction.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Zhang Min
AU  - Liang Zhan Ping
AU  - Huang Zhen Jiang
AU  - Tan Jun
PY  - 2015/09
DA  - 2015/09
TI  - Aircraft landing orbit design
BT  - Proceedings of the 2015 Conference on Informatization in Education, Management and Business
PB  - Atlantis Press
SP  - 253
EP  - 258
SN  - 2352-5398
UR  - https://doi.org/10.2991/iemb-15.2015.50
DO  - 10.2991/iemb-15.2015.50
ID  - Min2015/09
ER  -