Results 51 to 60 of about 1,814,382 (210)
In this paper, Active Disturbance Rejection Control (ADRC) is utilized in the attitude control of a quadrotor aircraft to address the problem of attitude destabilization in flight control caused by parameter uncertainties and external disturbances ...
Qi Zhang, Yaoxing Wei, Xiao Li
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Development of an Air-Bearing Testbed for Nanosatellite Attitude Determination and Control Systems
A testbed that simulates space conditions in a terrestrial laboratory is essential for evaluating, verifying, and teaching attitude control in nanosatellites.
Pablo Raul Yanyachi +3 more
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Attitude ground support system for the solar maximum mission spacecraft [PDF]
The SMM attitude ground support system (AGSS) supports the acquisition of spacecraft roll attitude reference, performs the in-flight calibration of the attitude sensor complement, supports onboard control autonomy via onboard computer data base updates ...
Nair, G.
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Integrated Suboptimal Guidance and Control for Lunar Pinpoint Soft Landing
It proposed an integrated guidance and control method for lunar pinpoint soft landing to deal with the mismatch between the guidance system and control system in conventional separating design philosophy.
ZHANG Bo, CAI Yuanli
doaj
This study studies the height and attitude tracking control problem of an unmanned helicopter system with disturbances. A composite controller based on the combination of harmonic disturbance observers and backstepping technique is proposed to achieve ...
Ling Han +3 more
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Attitude control system for sounding rockets Patent [PDF]
Development of attitude control system for sounding rocket stabilization during ballistic phase of ...
Robbins, H. J., Zebrowski, Z. E.
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This paper proposes an advanced model predictive control (MPC) scheme for the attitude tracking of coaxial drones under wind disturbances. Unlike most existing MPC setups, this scheme embeds steady-input, steady-output, and steady-state conditions into ...
Zhi Chen, Xiangyu Lin, Wanyue Jiang
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A backstepping-based robust adaptive fault tolerant control (FTC) scheme is proposed for the altitude and attitude dynamic model of the medium-scale unmanned autonomous helicopter (UAH) subjected to external disturbance and actuator fault.
Kun Yan +3 more
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Attitude control and damping system for spacecraft Patent [PDF]
Utilization of momentum devices for forming attitude control and damping system for ...
Kurzhals, P. R., Will, R. W.
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Tail-sitters aim to combine the advantages of fixed-wing aircraft and rotorcraft but require a robust and fast stabilization strategy to perform vertical maneuvers and transitions to and from aerodynamic flight.
Alexandre Athayde +2 more
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