| 发明名称 |
METHOD FOR ADAPTIVE ROLL CONTROL OF AIRCRAFT |
| 摘要 |
FIELD: aviation.SUBSTANCE: invention relates to a method of adaptive roll control of aircraft. For adaptive roll control of aircraft, method comprises estimating current aerodynamic parameters of transverse motion of aircraft, generating control signals monitoring change of quantity and arrangement of external suspensions compared with initial arrangement, calculating axial and centrifugal moments of inertia of aircraft adjusting aircraft control commands.EFFECT: higher stability and controllability of transverse motion of aircraft.1 cl, 1 dwg |
| 申请公布号 |
RU2600025(C2) |
申请公布日期 |
2016.10.20 |
| 申请号 |
RU20140142715 |
申请日期 |
2014.10.22 |
| 申请人 |
Federalnoe gosudarstvennoe kazennoe voennoe obrazovatelnoe uchrezhdenie vysshego professionalnogo obrazovaniya "Voennyj uchebno-nauchnyj tsentr Voenno-vozdushnykh sil "Voenno-vozdushnaya akademiya imeni professora N.E. ZHukovskogo i YU.A. Gagarina" (g. Voronezh) Ministerstva oborony Rossijskoj Federatsii |
发明人 |
Vereshshikov Dmitrij Viktorovich;Kostin Pavel Sergeevich;Vereshshagin YUrij Olegovich;Makarov Ilya Konstantinovich;Kuznetsov Aleksandr Dmitrievich |
| 分类号 |
G05D1/08;B64C19/00 |
主分类号 |
G05D1/08 |
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