Finite-time attitude stabilization for rigid spacecraft.
- Published in:
- International Journal of Robust & Nonlinear Control, 2015, v. 25, n. 1, p. 32, doi. 10.1002/rnc.3071
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- Publication type:
- Article
Works matching DE "SPACE vehicle dynamics"
Results: 23
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Effective Empirical Acceleration Modeling and its Application to Enhanced-Accuracy Orbit Prediction.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 39
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- Publication type:
- Article
3
Empirical Data Driven Model for Sail Membrane Dynamics Estimation.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 65
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- Publication type:
- Article
4
Near-Earth Asteroid Deflection Mission Using Coulomb Force Attractor.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 119
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- Publication type:
- Article
5
Spacecraft Attitude Control with RWs via LPV Control Theory: Comparison of Two Different Methods in One Framework.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 15
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- Publication type:
- Article
6
Flow Control by Repetitive Discharge for Space Vehicle at High Altitude.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 27
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- Publication type:
- Article
7
Estimation of dynamic characteristics of the International Space Station from measurements of microaccelerations.
- Published in:
- Cosmic Research, 2009, v. 47, n. 2, p. 173, doi. 10.1134/S0010952509020087
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- Publication type:
- Article
8
Stability of a rotating spacecraft partially filled with liquid: The case of several cavities.
- Published in:
- Cosmic Research, 2006, v. 44, n. 5, p. 433, doi. 10.1134/S0010952506050078
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- Publication type:
- Article
9
The influence of kinetics of neutral particles on near-surface glow of spacecraft.
- Published in:
- Cosmic Research, 2006, v. 44, n. 5, p. 425, doi. 10.1134/S0010952506050066
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- Publication type:
- Article
10
Rigid-elastic-thermal coupling dynamics and its application.
- Published in:
- Advances in Mechanical Engineering (Sage Publications Inc.), 2015, v. 7, n. 12, p. 1, doi. 10.1177/1687814015619766
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- Publication type:
- Article
11
Parametric excitation induced by solar pressure torque on the roll-yaw attitude motion of a gravity-gradient stabilized spacecraft.
- Published in:
- Celestial Mechanics & Dynamical Astronomy, 2010, v. 108, n. 4, p. 405, doi. 10.1007/s10569-010-9311-5
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- Publication type:
- Article
12
Analytical solutions for the equations of motion of a space vehicle during the atmospheric re-entry phase on a 2-D trajectory.
- Published in:
- Celestial Mechanics & Dynamical Astronomy, 2009, v. 103, n. 4, p. 327, doi. 10.1007/s10569-009-9199-0
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- Publication type:
- Article
13
OPTIMAL PRINCIPLE FOR DYNAMICAL SYSTEM WITH ALTERATIVE ORBITING.
- Published in:
- Electronics & Control Systems, 2016, v. 4, n. 50, p. 108, doi. 10.18372/1990-5548.50.11398
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- Publication type:
- Article
14
Missing part delays space mission.
- Published in:
- Nature, 2011, v. 469, n. 7330, p. 280, doi. 10.1038/469280a
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- Publication type:
- Article
15
Araç Dinamiği Modellenmesi, Simülasyonu ve Görselleştirilmesi.
- Published in:
- Journal of Defense Sciences / Savunma Bilmleri Dergisi, 2012, v. 11, n. 1, p. 133
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- Publication type:
- Article
16
Modelling of Spacecraft Dynamics at Deployment of Large Elastic Structure.
- Published in:
- Modelling & Simulation in Engineering, 2012, p. 1, doi. 10.1155/2012/497916
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- Publication type:
- Article
17
Chaotic oscillations of spacecraft with an elastic radially oriented tether.
- Published in:
- Cosmic Research, 2012, v. 50, n. 2, p. 188, doi. 10.1134/S0010952512020013
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- Publication type:
- Article
18
Survey of European andMajor ISC Facilities for Supporting Mars and Sample ReturnMission Aerothermodynamics and Tests Required for Thermal Protection System and Dynamic Stability.
- Published in:
- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/937629
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- Publication type:
- Article
19
Efficient Neural Network Modeling for Flight and Space Dynamics Simulation.
- Published in:
- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/247294
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- Publication type:
- Article
20
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
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- Publication type:
- Article
21
An Evolutionary Optimization Method for Designing a Thermal Protection System for Dynamics #.
- Published in:
- Mechanics Based Design of Structures & Machines, 2006, v. 34, n. 1, p. 1, doi. 10.1080/15397730600605944
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- Publication type:
- Article
22
Influence of Magnetically Conjugate Fragments of Auroral Emission Images on the Accuracy of Determining E<sub>av</sub> of Precipitating Electrons.
- Published in:
- Russian Physics Journal, 2018, v. 61, n. 1, p. 150, doi. 10.1007/s11182-018-1378-6
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- Publication type:
- Article
23
Analytical and Experimental Study Using Output-Only Modal Testing for On-Orbit Satellite Appendages.
- Published in:
- Advances in Acoustics & Vibration, 2009, v. 2009, p. 1, doi. 10.1155/2009/538731
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- Publication type:
- Article