В.А. Соловьёв, В.Е. Любинский, В.В. Ивашкин
16
Инженерный журнал: наука и инновации
# 9·2016
Control of manned space complex flight
for mission to asteroid
© V.A. Solovyov
1,3
, V.E. Lyubinskiy
1,3
, V.V. Ivashkin
2,3
1
S.P. Korolev Rocket and Space Public Corporation Energia,
Korolev, Moscow region, 141070, Russia
2
Keldysh Institute of Applied Mathematics, Moscow, 125047, Russia
3
Bauman Moscow State Technical University, Moscow, 105005, Russia
Currently the society considers relevant manned missions to asteroids. One of the objec-
tives of the flights to these bodies is to refine their shape, weight, rotation parameters,
material composition, their origin; do the analysis of their practical use. Another goal is
to protect the Earth from collision with the
"
dangerous
"
bodies, which could lead to dis-
aster. The asteroid Apophis belongs to this group. The study proposes the concept of a
possible manned mission to the
"
dangerous
"
body. We analyzed different ways to impact
the asteroid, considered the possible spaceship structures, and suggested the program of
the expedition, flight scheme and ship maneuvers near the asteroid. We examine space-
craft flight control issues at different stages of the expedition
.
Keywords:
human space flight, interplanetary flights, asteroids, asteroid-comet hazard,
interplanetary manned spacecraft, interplanetary trajectory, ballistics navigation sup-
port, flight control
.
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