Works matching DE "ARTIFICIAL satellite control systems"

Results: 27

Finite Element Analysis of Vibration Amplification Distribution in Lean Satellites.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 51

By:

Amgalanbat BATSUREN;
Toru HATAMURA;
Hirokazu MASUI;
Mengu CHO

Publication type:

Article

A Practical Rapid Attitude Maneuver Control System using Control Moment Gyros for Microsatellite TSUBAME.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2015, v. 13, n. 2015, p. 37, doi. 10.2322/tastj.13.37

By:

Ting HAO;
Shota KAWAJIRI;
Kyosuke TAWARA;
Saburo MUTUNAGA

Publication type:

Article

THE SWARM ARCHIVING PAYLOAD DATA FACILITY, AN INSTANCE CONFIGURATION OF THE ESA MULTI-MISSION FACILITY.

Published in:

International Archives of the Photogrammetry, Remote Sensing & Spatial Information Sciences, 2015, v. 40-7/W3, p. 685, doi. 10.5194/isprsarchives-XL-7-W3-685-2015

By:

Pruin, B.;
Martini, A.;
Shanmugam, P.;
Lopes, C.

Publication type:

Article

Nanosatellite REFLECTOR: Choice of parameters of the attitude control system.

Published in:

Cosmic Research, 2007, v. 45, n. 1, p. 60, doi. 10.1134/S0010952507010078

By:

Ovchinnikov, M. Yu.;
Shargorodskiy, V. D.;
Penkov, V. I.;
Mirer, S. A.;
Guerman, A. D.;
Nemuchinskiy, R. B.

Publication type:

Article

Averaged model to study long-term dynamics of a probe about Mercury.

Published in:

Celestial Mechanics & Dynamical Astronomy, 2018, v. 130, n. 2, p. 1, doi. 10.1007/s10569-017-9801-9

By:

Tresaco, Eva;
Carvalho, Jean Paulo S.;
Prado, Antonio F. B. A.;
Elipe, Antonio;
de Moraes, Rodolpho Vilhena

Publication type:

Article

SUM-SINES EQUATION FOR ESTIMATING THE PERCENT OF SHADOW LENGTH OF TARGETS IN THE SATELLITE IMAGES.

Published in:

Kufa Journal of Engineering, 2018, v. 9, n. 3, p. 112, doi. 10.30572/2018/kje/090309

By:

Ali, Shurooq Mahdi;
Al-Helaly, Emad Ali

Publication type:

Article

Deterministic and Recursive Approach in Attitude Determination for InnoSAT.

Published in:

Telkomnika, 2011, v. 9, n. 3, p. 583, doi. 10.12928/telkomnika.v9i3.752

By:

Fadly, M.;
Sidek, Othman;
Said, Md Azlin Md;
Djojodihardjo, Harijono;
Ain, Adam

Publication type:

Article

A Cross-Layer Rate Control Mechanism for Link-Adaptive Satellite Integrated Services.

Published in:

Research Letters in Signal Processing, 2007, p. 1, doi. 10.1155/2007/85937

By:

Gardikis, G.;
Kourtis, A.

Publication type:

Article

Cost optimization for maintaining the survivability of terrestrial objects of a satellite control system.

Published in:

Solar System Research, 2011, v. 45, n. 7, p. 641, doi. 10.1134/S0038094611070112

By:

Khokhlachev, E.

Publication type:

Article

MODELLING THE HIPPARCOS ATTITUDE.

Published in:

EAS Publications Series, 2010, v. 45, p. 41, doi. 10.1051/eas/1045007

By:

van Leeuwen, F.

Publication type:

Article

Accounting of fundamental components of the rotation parameters of the Earth in the formation of a high-accuracy orbit of navigation satellites.

Published in:

Doklady Physics, 2012, v. 57, n. 7, p. 276, doi. 10.1134/S1028335812070026

By:

Markov, Yu.;
Mikhailov, M.;
Pochukaev, V.

Publication type:

Article

Research and development techniques for early-warning satellite systems using concurrent engineering.

Published in:

Concurrent Engineering: Research & Applications, 2018, v. 26, n. 3, p. 215, doi. 10.1177/1063293X18768668

By:

Sun, Fuyu;
Wang, Hua;
Zhou, Jianping

Publication type:

Article

Nonlinear automatic control of the satellites by using the quaternion and the angular velocities' vectors.

Published in:

INCAS Bulletin, 2015, v. 7, n. 2, p. 93, doi. 10.13111/2066-8201.2015.7.2.9

By:

LUNGU, Romulus;
LUNGU, Mihai;
IOAN, Mihai

Publication type:

Article

Instantaneous Triple-Frequency GPS Cycle-Slip Detection and Repair.

Published in:

International Journal of Navigation & Observation, 2009, p. 1, doi. 10.1155/2009/407231

By:

Zhen Dai;
Knedlik, Stefan;
Loffeld, Otmar

Publication type:

Article

New Characteristics of Geometric Dilution of Precision (GDOP) for Multi-GNSS Constellations.

Published in:

Journal of Navigation, 2014, v. 67, n. 6, p. 1018, doi. 10.1017/S037346331400040X

By:

Teng, Yunlong;
Wang, Jinling

Publication type:

Article

Optimized synthesis of cost‐effective, controllable oil system architectures for turbofan engines.

Published in:

Systems Engineering, 2018, v. 21, n. 5, p. 417, doi. 10.1002/sys.21430

By:

Hambley, Christopher J.;
Jones, Bryn L.;
Griffin, Ian;
Mills, Andrew R.;
Kadirkamanathan, Visakan

Publication type:

Article

Applying autonomy to distributed satellite systems: Trends, challenges, and future prospects.

Published in:

Systems Engineering, 2018, v. 21, n. 5, p. 401, doi. 10.1002/sys.21428

By:

Araguz, Carles;
Bou‐Balust, Elisenda;
Alarcón, Eduard

Publication type:

Article

Multi-Scenarios Attitude Control of a Satellite with Flexible Solar Panels.

Published in:

International Review of Automatic Control, 2018, v. 11, n. 6, p. 326, doi. 10.15866/ireaco.v11i6.15266

By:

Khorchef, N.;
Mokhtari, A.;
Boudjemai, A.

Publication type:

Article

ADCS development for student CubeSat satellites -- TalTech case study.

Published in:

Proceedings of the Estonian Academy of Sciences, 2021, v. 70, n. 3, p. 268, doi. 10.3176/proc.2021.3.06

By:

Rassõlkin, Anton;
Vaimann, Toomas;
Org, Peeter;
Leibak, Alar;
Gordon, Rauno;
Priidel, Eiko

Publication type:

Article

LARES: A New Satellite Specifically Designed for Testing General Relativity.

Published in:

International Journal of Aerospace Engineering, 2015, v. 2015, p. 1, doi. 10.1155/2015/341384

By:

Paolozzi, Antonio;
Ciufolini, Ignazio;
Paris, Claudio;
Sindoni, Giampiero

Publication type:

Article

MILITARY SATELLITES: COMBINED COMMUNICATIONS GATEWAY GERALDTON.

Published in:

Asia-Pacific Defence Reporter, 2016, v. 42, n. 9, p. 24

By:

SLOCOMBE, GEOFF

Publication type:

Article

Pulse-width control of satellite during initial stop of its rotation and a station-keeping on sun-synchronous orbit.

Published in:

Mathematics in Engineering, Science & Aerospace (MESA), 2017, v. 8, n. 1, p. 65

By:

Somov, Sergey;
Butyrin, Sergey;
Somov, Yevgeny

Publication type:

Article

Guidance and adaptive-robust attitude & orbit control of a maneuvering information satellite.

Published in:

Mathematics in Engineering, Science & Aerospace (MESA), 2017, v. 8, n. 1, p. 53

By:

Somov, Yevgeny;
Butyrin, Sergey;
Somov, Sergey;
Somova, Tatyana;
Testoyedov, Nikolay;
Rayevsky, Valentine;
Titov, Gennady;
Yakimov, Yevgeny;
Ovchinnikov, Andrey;
Mathylenko, Mikhail

Publication type:

Article

Universal adaptive control of satellite formation flying.

Published in:

International Journal of Control, 2005, v. 78, n. 1, p. 45, doi. 10.1080/00207170412331330887

By:

Pongvthithum, R.;
Veres, S. M.;
Gabriel, S. B.;
Rogers, E.

Publication type:

Article

REFERENCE MODEL VARIABLE STRUCTURE OUTPUT FEEDBACK FOR ATTITUDE MANEUVERS CONTROL OF FLEXIBLE SPACECRAFTS.

Published in:

Intelligent Automation & Soft Computing, 2009, v. 15, n. 1, p. 53, doi. 10.1080/10798587.2009.10643015

By:

Qinglei Hu;
Xiao-Zhi Gao;
Guangfu Ma

Publication type:

Article

Global navigation satellite system and augmentation.

Published in:

Resonance: Journal of Science Education, 2017, v. 22, n. 12, p. 1155, doi. 10.1007/s12045-017-0579-6

By:

Swamy, K

Publication type:

Article

Application of the state-dependent riccati equation and kalman filter techniques to the design of a satellite control system.

Published in:

Shock & Vibration, 2012, v. 19, n. 5, p. 939, doi. 10.1155/2012/716975

By:

Souza, L.C.G.;
Gonzáles, R.G.

Publication type:

Article