Works matching DE "ARTIFICIAL satellite control systems"
Results: 26
Application of the state-dependent riccati equation and kalman filter techniques to the design of a satellite control system.
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- Shock & Vibration, 2012, v. 19, n. 5, p. 939, doi. 10.1155/2012/716975
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Cost optimization for maintaining the survivability of terrestrial objects of a satellite control system.
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- Solar System Research, 2011, v. 45, n. 7, p. 641, doi. 10.1134/S0038094611070112
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REFERENCE MODEL VARIABLE STRUCTURE OUTPUT FEEDBACK FOR ATTITUDE MANEUVERS CONTROL OF FLEXIBLE SPACECRAFTS.
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- Intelligent Automation & Soft Computing, 2009, v. 15, n. 1, p. 53, doi. 10.1080/10798587.2009.10643015
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Finite Element Analysis of Vibration Amplification Distribution in Lean Satellites.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 51
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A Practical Rapid Attitude Maneuver Control System using Control Moment Gyros for Microsatellite TSUBAME.
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- 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
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Accounting of fundamental components of the rotation parameters of the Earth in the formation of a high-accuracy orbit of navigation satellites.
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- Doklady Physics, 2012, v. 57, n. 7, p. 276, doi. 10.1134/S1028335812070026
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ADCS development for student CubeSat satellites -- TalTech case study.
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- Proceedings of the Estonian Academy of Sciences, 2021, v. 70, n. 3, p. 268, doi. 10.3176/proc.2021.3.06
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Instantaneous Triple-Frequency GPS Cycle-Slip Detection and Repair.
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- International Journal of Navigation & Observation, 2009, p. 1, doi. 10.1155/2009/407231
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Global navigation satellite system and augmentation.
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- Resonance: Journal of Science Education, 2017, v. 22, n. 12, p. 1155, doi. 10.1007/s12045-017-0579-6
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Research and development techniques for early-warning satellite systems using concurrent engineering.
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- Concurrent Engineering: Research & Applications, 2018, v. 26, n. 3, p. 215, doi. 10.1177/1063293X18768668
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Optimized synthesis of cost‐effective, controllable oil system architectures for turbofan engines.
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- Systems Engineering, 2018, v. 21, n. 5, p. 417, doi. 10.1002/sys.21430
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Applying autonomy to distributed satellite systems: Trends, challenges, and future prospects.
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- Systems Engineering, 2018, v. 21, n. 5, p. 401, doi. 10.1002/sys.21428
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Multi-Scenarios Attitude Control of a Satellite with Flexible Solar Panels.
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- International Review of Automatic Control, 2018, v. 11, n. 6, p. 326, doi. 10.15866/ireaco.v11i6.15266
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MILITARY SATELLITES: COMBINED COMMUNICATIONS GATEWAY GERALDTON.
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- Asia-Pacific Defence Reporter, 2016, v. 42, n. 9, p. 24
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Universal adaptive control of satellite formation flying.
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- International Journal of Control, 2005, v. 78, n. 1, p. 45, doi. 10.1080/00207170412331330887
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A Cross-Layer Rate Control Mechanism for Link-Adaptive Satellite Integrated Services.
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- Research Letters in Signal Processing, 2007, p. 1, doi. 10.1155/2007/85937
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THE SWARM ARCHIVING PAYLOAD DATA FACILITY, AN INSTANCE CONFIGURATION OF THE ESA MULTI-MISSION FACILITY.
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- 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
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Nanosatellite REFLECTOR: Choice of parameters of the attitude control system.
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- Cosmic Research, 2007, v. 45, n. 1, p. 60, doi. 10.1134/S0010952507010078
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SUM-SINES EQUATION FOR ESTIMATING THE PERCENT OF SHADOW LENGTH OF TARGETS IN THE SATELLITE IMAGES.
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- Kufa Journal of Engineering, 2018, v. 9, n. 3, p. 112, doi. 10.30572/2018/kje/090309
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MODELLING THE HIPPARCOS ATTITUDE.
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- EAS Publications Series, 2010, v. 45, p. 41, doi. 10.1051/eas/1045007
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New Characteristics of Geometric Dilution of Precision (GDOP) for Multi-GNSS Constellations.
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- Journal of Navigation, 2014, v. 67, n. 6, p. 1018, doi. 10.1017/S037346331400040X
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Guidance and adaptive-robust attitude & orbit control of a maneuvering information satellite.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2017, v. 8, n. 1, p. 53
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Pulse-width control of satellite during initial stop of its rotation and a station-keeping on sun-synchronous orbit.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2017, v. 8, n. 1, p. 65
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LARES: A New Satellite Specifically Designed for Testing General Relativity.
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- International Journal of Aerospace Engineering, 2015, v. 2015, p. 1, doi. 10.1155/2015/341384
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Averaged model to study long-term dynamics of a probe about Mercury.
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- Celestial Mechanics & Dynamical Astronomy, 2018, v. 130, n. 2, p. 1, doi. 10.1007/s10569-017-9801-9
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Nonlinear automatic control of the satellites by using the quaternion and the angular velocities' vectors.
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- INCAS Bulletin, 2015, v. 7, n. 2, p. 93, doi. 10.13111/2066-8201.2015.7.2.9
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