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Н.Е. Зубов, В.Н. Рябченко, М.Н. Поклад, Д.Е. Ефанов, Е.И. Старовойтов
12
Инженерный журнал: наука и инновации
# 5·2017
Universal control laws of stabilizing longitudinal motion
of different types of aircrafts
© N.E. Zubov
1,2
, V.N. Ryabchenko
2
, М.N. Poklad
2
,
D.E. Efanov
1
, Е.I. Starovoytov
1
1
S.P. Korolev Rocket and Space Public Corporation Energia,
Korolev town, Moscow region, 141070, Russia
2
Bauman Moscow State Technical University, Moscow, 105005, Russia
The paper presents the analytically synthesized law of lateral movement stabilization. It
is done for the linearized model of the fourth order lateral movement of an isolated sin-
gle-rotor helicopter, which can be regarded as a universal model for the aircraft lateral
movement of any type and which represents the MIMO system containing two entrances.
The decomposition method of MIMO system modal control, which was previously devel-
oped by the authors, is the basis of the decomposition synthesis. To check the correctness
of the problem, we perform mathematical modeling of the single-rotor helicopter lateral
movement using stabilization laws synthesized analytically. We present graphs of transi-
ent processes of the helicopter lateral movement as well as component changes of the
vector control during the implementation process of the synthesized control laws.
Keywords:
MIMO-system, decomposition, analytical synthesis, longitudinal movement of
aircrafts, dynamic system poles, control matrix
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