Optimization of the hierarchical system of "guidance-stabilization" of the aircraft with the stabilization system adaptation
Authors: Vanin A.V., Voronov E.M., Serov V.A., Karpunin A.A., Lyubavskiy K.K. | Published: 03.09.2015 |
Published in issue: #4(103)/2015 | |
DOI: 10.18698/0236-3933-2015-4-13-33 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
Keywords: control optimization, hierarchical systems, coordination, executive control, guidance, stabilization, aircraft |
Problem solution of averaging orbital motion parameters of the International space station during conducting the space experiment Global Transmission Services 2
Authors: Mikrin E.A., Sumarokov A.V., Zubov N.E., Ryabchenko V.N. | Published: 12.10.2015 |
Published in issue: #5(104)/2015 | |
DOI: 10.18698/0236-3933-2015-5-3-17 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
Keywords: International space station, space experiments, Global Transmission Services, state vector, orbital motion, dynamic filtration |
Static analysis techniques for electrohydraulic control actuators of rocket packs
Authors: Belonogov O.B. | Published: 12.10.2015 |
Published in issue: #5(104)/2015 | |
DOI: 10.18698/0236-3933-2015-5-18-29 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Control and Testing of Aircrafts and their Systems | |
Keywords: static analysis, control actuator, numerical integration, nonlinear differential equations |
Algorithm for computing program values of angular velocity vector components during spacecraft terminal spatial turn in the inertial coordinate system
Authors: Zubov N.E., Li E.K., Li M.V., Mikrin E.A., Poklad M.N., Ryabchenko V.N. | Published: 23.12.2015 |
Published in issue: #6(105)/2015 | |
DOI: 10.18698/0236-3933-2015-6-3-20 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
Keywords: kinematic equations, quaternions, boundary value problem, modal control, identification |
Integral criterion for determining the existence domain of periodic orbits in the vicinity of a smaller body in three-body problem
Authors: Zvyagin F.V., Lysenko L.N. | Published: 23.12.2015 |
Published in issue: #6(105)/2015 | |
DOI: 10.18698/0236-3933-2015-6-21-29 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
Keywords: elliptic restricted three-body problem, F-orbits, periodic orbits, Lyapunov orbits, integral criterion, principle of least action |
Application of bulk high-temperature superconductors in advanced space systems
Authors: Matveev V.A. , Maevskiy V.A., Aseev V.V., Ivlev A.S., Sysoev M.A. | Published: 19.02.2016 |
Published in issue: #1(106)/2016 | |
DOI: 10.18698/0236-3933-2016-1-15-32 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Innovation Technologies in Aerospace Activity | |
Keywords: bulk high-temperature superconductor, permanent magnet, space object, cryovacuum system |
Parameterization of analytic control laws for aircraft lateral motion
Authors: Zubov N.E., Mikrin E.A., Ryabchenko V.N., Poklad M.N. | Published: 08.04.2016 |
Published in issue: #2(107)/2016 | |
DOI: 10.18698/0236-3933-2016-2-3-17 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
Keywords: decomposition, modal synthesis, MIMO-system, aircraft lateral motion, dynamical system pole, parameterization |
Low level reservation of the hardware architecture of reconfigurable complex functional monitoring and diagnostics system of the onboard spacecraft control
Authors: Savkin L.V., Novichkov V.M., Shirshakov A.E. | Published: 08.04.2016 |
Published in issue: #2(107)/2016 | |
DOI: 10.18698/0236-3933-2016-2-18-27 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Control and Testing of Aircrafts and their Systems | |
Keywords: onboard control complex, majority reservation, reconfigurable computing field |
The research into correction algorithms for aircraft navigation systems
Authors: Shen Kai, Proletarsky A.V., Neusypin K.A. | Published: 08.04.2016 |
Published in issue: #2(107)/2016 | |
DOI: 10.18698/0236-3933-2016-2-28-39 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
Keywords: aircraft, navigation complex, nonlinear Kalman filter, self-organization algorithm, genetic algorithm |
Engineering method integrated with CAD-system for optimizing the horizontal empennage parameters of the maneuverable aircraft
Authors: Romanova T.N., Paschenko O.B., Gavrilova N.Yu., Schetinin G.A. | Published: 08.04.2016 |
Published in issue: #2(107)/2016 | |
DOI: 10.18698/0236-3933-2016-2-40-52 | |
Category: Aviation, Rocket and Space Engineering | Chapter: Innovation Technologies in Aerospace Activity | |
Keywords: CAD-system, CAE-system, multi-objective optimization, horizontal aircraft empennage, moment of the horizontal empennage |