## Found 736 Documents (Results 1–100)

100
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### A dimension-reduction method for the finite-horizon spacecraft pursuit-evasion game. (English)Zbl 07616040

MSC:  58F15 58F17 53C35
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MSC:  93C95
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### Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft. (English)Zbl 07595546

MSC:  93B12 70M20
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MSC:  70-XX
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### Fully-actuated system approach based optimal attitude tracking control of rigid spacecraft with actuator saturation. (English)Zbl 1495.93056

MSC:  93C85 93C20
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### Attitude and orbit optimal control of combined spacecraft via a fully-actuated system approach. (English)Zbl 1495.93061

MSC:  93C95 49N10
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### Attitude control of spherical liquid-filled spacecraft based on high-order fully actuated system approaches. (English)Zbl 1495.93062

MSC:  93C95 70P05
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### Fixed-time sliding mode attitude control of a flexible spacecraft with rotating appendages connected by magnetic bearing. (English)Zbl 1489.93019

MSC:  93B12 93C95
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### Schemes of momentum/reaction wheels unloading by mechanical restructuring and gearbox for spacecraft. (English)Zbl 1483.70043

MSC:  70Q05 70B15
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### A characteristic modeling method of error-free compression for nonlinear systems. (English)Zbl 1490.93055

MSC:  93C10 93C35
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### Optimal orientation control of a space vehicle with restrictions on the control and phase variables. (English. Russian original)Zbl 1487.49058

J. Comput. Syst. Sci. Int. 60, No. 6, 1027-1045 (2021); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2021, No. 6, 158-176 (2021).
MSC:  49S05 49K21
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### Studying the accuracy of forecasting electric power generation by solar panels of the Zarya service module on the international space station using a mathematical model. (English. Russian original)Zbl 1484.78010

Mosc. Univ. Comput. Math. Cybern. 45, No. 4, 180-190 (2021); translation from Vestn. Mosk. Univ., Ser. XV 2021, No. 4, 43-52 (2021).
MSC:  78A55 78A40 65K10
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### Optimisation of controller reconfiguration instant for spacecraft control systems with additive actuator faults. (English)Zbl 1483.49008

MSC:  49J10 70M20
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### Restore relative spaceship trajectory during approacing to the space station using mathematic model. (Russian. English translation)Zbl 1495.70014

Mat. Model. 33, No. 11, 77-94 (2021); translation in Math. Models Comput. Simul. 14, No. 3, 490-502 (2022).
MSC:  70M20
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MSC:  70E60
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### Finite time distributed coordinated control for attitude of multi-spacecraft based on super-twisting algorithm. (Chinese. English summary)Zbl 1488.93028

MSC:  93B12 93D40 93B53
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### Determining the parameters of a mathematical model of spacecraft solar batteries from telemetry data. (English. Russian original)Zbl 07441911

Mosc. Univ. Comput. Math. Cybern. 45, No. 3, 120-125 (2021); translation from Vestn. Mosk. Univ., Ser. XV 2021, No. 3, 37-43 (2021).
MSC:  65Kxx 90Cxx 90-XX
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### Nonlinear optimal approach to spacecraft formation flying using Lorentz and impulsive actuation. (English)Zbl 1481.49026

MSC:  49L12 49N25 49S05
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MSC:  49J10
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### Anti-unwinding sliding mode attitude control via two modified Rodrigues parameter sets for spacecraft. (English)Zbl 1478.93088

MSC:  93B12 70M20
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### Chebyshev neural network-based attitude-tracking control for rigid spacecraft with finite-time convergence. (English)Zbl 1478.93089

MSC:  93B12 93C95 70M20
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MSC:  70F07
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### Mathematic modeling of spacecraft solar panels. (Russian. English translation)Zbl 1494.78015

Mat. Model. 33, No. 9, 87-107 (2021); translation in Math. Models Comput. Simul. 14, No. 2, 322-334 (2022).
MSC:  78A55 78A05 78-10
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### Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional. (English. Russian original)Zbl 1475.49023

Autom. Remote Control 82, No. 7, 1183-1200 (2021); translation from Avtom. Telemekh. 2021, No. 7, 86-106 (2021).
MSC:  49K15 49K21
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### Sliding-mode-observer-based time-varying formation tracking for multispacecrafts subjected to switching topologies and time-delays. (English)Zbl 1471.93067

MSC:  93B12 93A16
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### Floquet modes and stability analysis of periodic orbit-attitude solutions along Earth-Moon halo orbits. (English)Zbl 1472.70023

MSC:  70F07 70K20 70M20
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### Finite-time adaptive robust control for SGCMGs-based flexible spacecraft. (Chinese. English summary)Zbl 1474.93055

MSC:  93B35 93C40
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### Analytical algorithm of energy and time quasioptimal turn of a spacecraft under arbitrary boundary conditions. (Russian. English summary)Zbl 1464.70019

MSC:  70M20 70Q05
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### The dynamics characteristics of flexible spacecraft and its closed-loop stability with passive control. (English)Zbl 1460.93075

MSC:  93D05 93B18 93B52
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### Foundations of space dynamics. (English)Zbl 1484.70025

Aerospace Series. Hoboken, NJ: John Wiley & Sons (ISBN 978-1-119-45534-9/pbk; 978-1-119-45530-1/ebook). xiii, 352 p. (2021).
MSC:  70M20 70-01
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### Fixed-time control for high-precision attitude stabilization of flexible spacecraft. (English)Zbl 1455.93099

MSC:  93C40 93B12
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### Mathematical modeling and simulation of nonlinear spacecraft rendezvous and formation flying problems via averaging method. (English)Zbl 1466.70037

MSC:  70M20 34C29 70E55
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### Neural adaptive integral sliding mode control for attitude tracking of flexible spacecraft with signal quantisation and actuator nonlinearity. (English)Zbl 1483.93292

MSC:  93C40 93B12 70M20
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MSC:  70M20
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### An off-policy approach for model-free stabilization of linear systems subject to input energy constraint and its application to spacecraft rendezvous. (English)Zbl 1467.93252

MSC:  93D15 93C95 93C05
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### Fixed-time attitude tracking control for spacecraft based on adding power integrator technique. (English)Zbl 1465.93105

MSC:  93C40 93D40 93C95
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### Finite-time attitude-tracking control for rigid spacecraft with actuator failures and saturation constraints. (English)Zbl 1465.93186

MSC:  93D40 93B12 93C42
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### The Lyapunov function nonlinear attitude control of under-actuated spacecraft. (Chinese. English summary)Zbl 1474.93192

MSC:  93D30 93C10
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### Attitude trajectory planning and attitude control for quad-rotor aircraft based on finite-time control technique. (English)Zbl 07323503

MSC:  70Q05 93D05
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### Methodology of intelligent analysis and forecasting for the state of resources in the Russian segment of the international space station based on digital identification models. (English. Russian original)Zbl 1454.93159

Autom. Remote Control 81, No. 9, 1692-1701 (2020); translation from Avtom. Telemekh. 2020, No. 9, 160-172 (2020).
MSC:  93C62 93C95
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### Comparison of two models of the force of aerodynamic drag for determining the orbital motion of the International Space Station. (Russian. English translation)Zbl 1493.70086

Mat. Model. 32, No. 10, 77-90 (2020); translation in Math. Models Comput. Simul. 13, No. 3, 502-511 (2021).
MSC:  70M20
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### Sensitivity of the gravity assist to variations of the impact parameter. (English)Zbl 1454.83013

MSC:  83C10 70F15 85A05
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### Distributed fixed-time attitude coordination control for multiple rigid spacecraft. (English)Zbl 1451.93009

MSC:  93A14 93C95 93B53
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### Attitude estimation based on robust information cubature quaternion filter. (English)Zbl 1448.93334

MSC:  93E11 93B35 93C95
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### Robust attitude alignment in multispacecraft systems with stochastic links failure. (English)Zbl 1447.93074

MSC:  93B35 93D50 93C95
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### Construction of interactive geometric model of outside surface of a spacecraft. (Russian. English summary)Zbl 1470.70038

MSC:  70P99 65D17
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MSC:  70M20
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### Attitude control of rigid spacecraft with predefined-time stability. (English)Zbl 1437.93097

MSC:  93C95 93D99 93B12
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### Fixed-time attitude tracking control for rigid spacecraft. (English)Zbl 1440.93136

MSC:  93C85 70Q05
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### Analysis on reachable set for spacecraft relative motion under low-thrust. (English)Zbl 1436.93015

MSC:  93B03 93C25 93C95
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### Inertial navigation in space using the regular quaternion equations of astrodynamics. (English. Russian original)Zbl 1465.70013

Mech. Solids 54, No. 2, 157-168 (2019); translation from Prikl. Mat. Mekh. 82, No. 6, 706-720 (2018).
MSC:  70E15 85A05
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### Chaotic motion and control of a tethered-sailcraft system orbiting an asteroid. (English)Zbl 1466.70032

MSC:  70M20 70K55 37D45
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MSC:  70F07
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### Satellite with periodical mass redistribution: relative equilibria and their stability. (English)Zbl 1448.70086

MSC:  70P05 70E55 70M20
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### 6-DOF fixed-time adaptive tracking control for spacecraft formation flying with input quantization. (English)Zbl 1448.93163

MSC:  93C40 93B12 93C95
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MSC:  94C12

### Fault diagnosability evaluation of deep space exploration spacecraft based on graph theory. (Chinese. English summary)Zbl 1449.94090

MSC:  94C12 94C15

### Dynamic modeling and attitude control of flexible solar sail spacecraft for deep space exploration. (Chinese. English summary)Zbl 1449.93207

MSC:  93C95 93B52

### Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality. (English. Russian original)Zbl 1448.93087

J. Comput. Syst. Sci. Int. 58, No. 6, 980-1003 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 6, 139-162 (2019).
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### Analytical algorithm for constructing the orbital orientation of a spacecraft with an incomplete measurement of the state vector components. (English. Russian original)Zbl 1448.93089

J. Comput. Syst. Sci. Int. 58, No. 6, 969-979 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 6, 128-138 (2019).
MSC:  93B50 93B53 93C95
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### Finite-time attitude control for rigid spacecraft subject to actuator saturation. (English)Zbl 1437.93103

MSC:  93D15 93D40 93C85
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### Fault-tolerant spacecraft attitude control under actuator saturation and without angular velocity. (English)Zbl 1447.93076

MSC:  93B35 93C95 93B52
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### Inertia-free attitude stabilization for flexible spacecraft with active vibration suppression. (English)Zbl 1447.93257

MSC:  93D05 93C95
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### Algorithm for controlling a spacecraft’s engine with preventing the angular momentum accumulation. (English. Russian original)Zbl 1440.93181

J. Comput. Syst. Sci. Int. 58, No. 5, 801-810 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 5, 145-154 (2019).
MSC:  93C95 93C27
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### Distributed adaptive fault-tolerant attitude tracking of multiple flexible spacecraft on $$\mathrm{SO}(3)$$. (English)Zbl 1432.70047

MSC:  70Q05 93C85 93D40
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### Calculation of program controls not generating singular states of a gyro system. II. (English. Russian original)Zbl 1432.93245

J. Comput. Syst. Sci. Int. 58, No. 3, 491-502 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 3, 164-176 (2019).
MSC:  93C95 93-08
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### Algorithms of stabilization of a spacecraft with flexible elements. (English. Russian original)Zbl 1432.93262

J. Comput. Syst. Sci. Int. 58, No. 3, 474-490 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 3, 147-163 (2019).
MSC:  93D05 93C95
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### Reconstruction of a spacecraft’s attitude motion using the data on the current collected from solar panels. (English. Russian original)Zbl 1432.93244

J. Comput. Syst. Sci. Int. 58, No. 2, 286-296 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 2, 133-144 (2019).
MSC:  93C95
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### Restricted quadratic optimal control of a spacecraft turning in a fixed time period. (English. Russian original)Zbl 1432.49069

J. Comput. Syst. Sci. Int. 58, No. 1, 126-146 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 1, 131-152 (2019).
MSC:  49S05 49K15 70G75
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### Optimal rotation of the orbit plane of a variable mass spacecraft in the central gravitational field by means of orthogonal thrust. (English. Russian original)Zbl 1431.93032

Autom. Remote Control 80, No. 8, 1437-1454 (2019); translation from Avtom. Telemekh. 2019, No. 8, 87-108 (2019).
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### Parametric multi-objective design for spacecrafts attitude control system with super flexible netted antennas. (Chinese. English summary)Zbl 1449.93058

MSC:  93B51 93B35 93B52
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### Data-driven-based attitude control of combined spacecraft with noncooperative target. (English)Zbl 1430.93157

MSC:  93C95 93B18 93D05
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### Event-triggered backstepping control for attitude stabilization of spacecraft. (English)Zbl 1423.93260

MSC:  93C65 93D20 93C95
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### Robust stabilization of spacecraft attitude motion under magnetic control through time-varying integral sliding mode. (English)Zbl 1426.93252

MSC:  93D09 93B12 93C95
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