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A critical comparison on attitude estimation: From gaussian approximate filters to coordinate‐free dual optimal control.
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- IET Control Theory & Applications (Wiley-Blackwell), 2021, v. 15, n. 10, p. 1297, doi. 10.1049/cth2.12109
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- Article
A Fast Adaptive-Gain Complementary Filter Algorithm for Attitude Estimation of an Unmanned Aerial Vehicle.
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- Journal of Navigation, 2018, v. 71, n. 6, p. 1478, doi. 10.1017/S0373463318000231
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- Article
Fault diagnosis method for closed-loop satellite attitude control systems based on a fuzzy parity equation.
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- International Journal of Distributed Sensor Networks, 2018, v. 14, n. 10, p. 1, doi. 10.1177/1550147718805938
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- Article
Tracking differentiator and extended state observer-based nonsingular fast terminal sliding mode attitude control for a quadrotor.
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- Nonlinear Dynamics, 2018, v. 94, n. 1, p. 343, doi. 10.1007/s11071-018-4362-3
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- Article
Attitude control system proposed for SERPENS-2 space mission.
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- Computational & Applied Mathematics, 2018, v. 37, n. 4, p. 4743, doi. 10.1007/s40314-018-0574-x
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- Article
Harmonic Extended State Observer Based Anti-Swing Attitude Control for Quadrotor with Slung Load.
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- Electronics (2079-9292), 2018, v. 7, n. 6, p. 83, doi. 10.3390/electronics7060083
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- Article
Design and comparison of embedded air coils for small satellites.
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- Turkish Journal of Electrical Engineering & Computer Sciences, 2018, v. 26, n. 2, p. 1027, doi. 10.3906/elk-1701-112
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- Article
Spacecraft Anti‐Unwinding Attitude Control Using Second‐Order Sliding Mode.
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- Asian Journal of Control, 2018, v. 20, n. 1, p. 455, doi. 10.1002/asjc.1601
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- Article
Anti-disturbance fault-tolerant attitude control for satellites subject to multiple disturbances and actuator saturation.
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- Nonlinear Dynamics, 2017, v. 89, n. 4, p. 2657, doi. 10.1007/s11071-017-3614-y
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- Article
Anti-Unwinding Attitude Control with Fixed-Time Convergence for a Flexible Spacecraft.
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- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/5018323
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- Article
Full state-feedback solution for a flywheel based satellite energy and attitude control scheme.
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- Journal of Vibroengineering, 2017, v. 19, n. 5, p. 3522, doi. 10.21595/jve.2017.18066
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- Article
Observer-based attitude controller for lifting re-entry vehicle with non-minimum phase property.
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- International Journal of Advanced Robotic Systems, 2017, v. 14, n. 3, p. 1, doi. 10.1177/1729881417703953
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- Article
NANOSATELLITE ATTITUDE ESTIMATION FROM VECTOR MEASUREMENTS USING SVD-AIDED UKF ALGORITHM.
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- Metrology & Measurement Systems, 2017, v. 24, n. 1, p. 113, doi. 10.1515/mms-2017-0011
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- Article
FUZZY PID CONTROLLER FOR NANO-SATELLITE ATTITUDE CONTROL.
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- Journal of Science & Arts, 2016, v. 16, n. 4, p. 407
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- Article
Experimental research and numerical simulation on vibration characteristics of a rectangular plate structure in fast time-varying thermal environments.
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- Vibroengineering Procedia, 2016, v. 10, p. 28
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- Article
Incipient Fault Detection Using an Associated Adaptive and Sliding-Mode Observer for Quadrotor Helicopter Attitude Control Systems.
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- Circuits, Systems & Signal Processing, 2016, v. 35, n. 10, p. 3555, doi. 10.1007/s00034-015-0229-8
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- Article
Adaptive robust attitude control for UAVs - Design and experimental validation.
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- International Journal of Adaptive Control & Signal Processing, 2016, v. 30, n. 8-10, p. 1478, doi. 10.1002/acs.2630
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- Article
Wave-Based Attitude Control of Spacecraft with Fuel Sloshing Dynamics.
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- Archive of Mechanical Engineering, 2016, v. 63, n. 2, p. 263, doi. 10.1515/meceng-2016-0015
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- Article
A simple saturated control framework for spacecraft with bounded disturbances.
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- International Journal of Robust & Nonlinear Control, 2016, v. 26, n. 3, p. 367, doi. 10.1002/rnc.3303
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- Article
Attitude Estimation of Nano-satellite with Deployable Aeroshell during Orbital Decay.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 1
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- Article
Development and Flight Results of Microsatellite Bus System for RISING-2.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 89
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- Article
Improvement of Star Sensor in Generic Test Environment.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 97
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- Article
Design and Control of an Unmanned Aerial Vehicle for Autonomous Parcel Delivery with Transition from Vertical Take-off to Forward Flight-VertiKUL, a Quadcopter Tailsitter.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 4, p. 1, doi. 10.1260/1756-8293.7.4.395
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- Article
Finite-time attitude control of multiple rigid spacecraft using terminal sliding mode.
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- International Journal of Robust & Nonlinear Control, 2015, v. 25, n. 12, p. 1862, doi. 10.1002/rnc.3182
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- Article
IGSO Satellite Orbit Determining Strategy Analysis with the Yaw-steering and Orbit-normal Attitude Control Mode Switching.
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- Geomatics & Information Science of Wuhan University, 2014, v. 39, n. 11, p. 1352, doi. 10.13203/j.whugis20130236
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The results of flight tests of an attitude control system for the Chibis-M microsatellite.
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- Cosmic Research, 2014, v. 52, n. 3, p. 205, doi. 10.1134/S0010952514020038
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- Article
Global Observer-based Attitude Controller Using Direct Inertial Measurements.
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- International Journal of Advanced Robotic Systems, 2014, v. 11, n. 4, p. 1, doi. 10.5772/56861
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- Article
Satellite Attitude Control System Design Taking into Account the Fuel Slosh and Flexible Dynamics.
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- Mathematical Problems in Engineering, 2014, p. 1, doi. 10.1155/2014/820586
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Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach.
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- Modelling & Simulation in Engineering, 2014, p. 1, doi. 10.1155/2014/652571
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- Article
Robust attitude control of uncertain quadrotors.
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- IET Control Theory & Applications (Wiley-Blackwell), 2013, v. 7, n. 11, p. 1583, doi. 10.1049/iet-cta.2012.0964
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- Article
Antidisturbance Fault Tolerant Control of Attitude Control Systems for Microsatellite with Unknown Input Delay.
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- Mathematical Problems in Engineering, 2013, p. 1, doi. 10.1155/2013/804754
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- Article
Attitude Control of a Single Tilt Tri-Rotor UAV System: Dynamic Modeling and Each Channel's Nonlinear Controllers Design.
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- Mathematical Problems in Engineering, 2013, p. 1, doi. 10.1155/2013/275905
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- Article
Design of a nonlinear controller for a rigid-flexible satellite using multi-objective Generalized Extremal Optimization with real codification.
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- Shock & Vibration, 2012, v. 19, n. 5, p. 947, doi. 10.1155/2012/254895
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- Article
Attitude control system of the first Russian nanosatellite TNS-0 no. 1.
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- Cosmic Research, 2010, v. 48, n. 6, p. 517, doi. 10.1134/S0010952510060043
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Comparison Study on Low Cost Satellite Magnetic Attitude Control Options.
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- International Review of Aerospace Engineering, 2010, v. 3, n. 3, p. 157
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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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- Article