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Алгоритм выбора коэффициентов пропорционального метода наведения…
Инженерный журнал: наука и инновации
# 9·2016 15
Parameter selection algorithm for proportional navigation
aircraft guidance based on target position
© A.N. Klishin, O.S. Shvyrkina
Bauman Moscow State Technical University, Moscow, 105005, Russia
Employing aircraft guidance at the final trajectory span should ensure that the conse-
quences of previous manoeuvres along with deviations of real trajectory from nominal
homing trajectory are eliminated. At present, trajectory guidance methods do not com-
pletely satisfy the requirements for efficiently reaching ground targets. Therefore, devel-
oping algorithms of trajectory guidance to collectively increase accuracy and potential
stationary object reaching zone is a pressing problem. The primary objective of the study
is to synthesise and validate implementation of an object guidance algorithm based on
selecting proportional guidance parameters with the help of empirical dependences, so
that the algorithm makes it possible to execute the tasks posed. Guidance based on the
algorithm developed made it possible to improve guidance quality by increasing accura-
cy and expanding the target reaching zone threefold.
Keywords:
guidance methods, accuracy, aircraft.
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Klishin A.N.
(b. 1975) graduated from Bauman Moscow State Technical University in
1999. Assoc. Professor, Department of Dynamics and Flight Control of Rockets and
Spacecraft, Bauman Moscow State Technical University. Author of over 150 scientific
and popular science publications in the fields of ballistics, flight dynamics, aircraft mo-
tion guidance and armament history.
Shvyrkina O.S.
(b. 1992), a student, Department of Dynamics and Flight Control of
Rockets and Spacecraft, Bauman Moscow State Technical University.
e-mail:
bonjour15@mail.ru