Small-sized Integrated Navigation & Landing Complex

Navigation systems


Аuthors

Aleshin B. S.1, Antonov D. A.2*, Veremeenko K. K.3, Zharkov M. V.2**, Zimin R. Y.4, Kuznetsov I. M.2***, Pron'kin A. N.2****

1. ,
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
3. ,
4. ,

*e-mail: oxface@yandex.ru
**e-mail: mv_zharkov@mai.ru
***e-mail: im_kuznetsov@mai.ru
****e-mail: an.pronkin@gmail.com

Abstract

One of possible approaches of working out of a small-sized integrated navigation & landing complex for an unmanned aerial vehicle is presented. The construction concept, design, and software of the complex are considered. An example of working out of a small-sized onboard navigation & landing complex based on the suggested approach and results of its flight tests are resulted.

Keywords:

unmanned aerial vehicle, inertial navigation system, MEMS, global navigation system, magnetic compass, the system of air signals, the optimal processing of information, integrated navigation system.


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