Results 11 to 20 of about 213,618 (168)

Design of the RLG Current Stabilizer Circuit for Attitude Control in the Satellite [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2006
In this paper, we describe the RLG current stabilizer circuit for attitude control in the satellite. The RLG makes use of the Sagnac effect within a resonant of a HeNe laser.
Eui-Chan Kim, Jae-Dong Choi
doaj   +1 more source

Attitude control of a tethered spacecraft

open access: yesProceedings of the 2003 American Control Conference, 2003., 2004
An attitude control problem for a tethered spacecraft is studied. The tethered spacecraft is viewed as a multi-body spacecraft consisting of a base body, a massless tether that connects the base body and an end mass, and tether actuator dynamics. Moments about the pitch and roll axes of the base spacecraft arise by control of the point of attachment of
Sangbum Cho, N. Harris McClamroch
openaire   +2 more sources

Monoaxial Electrodynamic Stabilization of an Artificial Earth Satellite in the Orbital Coordinate System via Control With Distributed Delay

open access: yesIEEE Access, 2021
An artificial Earth satellite (AES) with three different principal central moments of inertia is under consideration. The AES moves along a Keplerian circular equatorial near-Earth orbit.
Alexander Aleksandrov   +1 more
doaj   +1 more source

A Novel Disturbance Rejection Control of Roll Channel for Small Air-to-Surface Missiles

open access: yesApplied Sciences, 2022
In this paper, the issue of roll channel for attitude control for small air-to-surface missiles suffering from multiple disturbances is investigated. The dynamic model of roll channel is established and the roll controller of roll channel based on the ...
Xiaomiao Ding   +3 more
doaj   +1 more source

Error Dynamics Based Dual Heuristic Dynamic Programming for Self-Learning Flight Control

open access: yesApplied Sciences, 2022
A data-driven nonlinear control approach, called error dynamics-based dual heuristic dynamic programming (ED-DHP), is proposed for air vehicle attitude control. To solve the optimal tracking control problem, the augmented system is defined by the derived
Xu Huang   +5 more
doaj   +1 more source

Path-Following Control for Unmanned Surface Vessel Using 1st System of Identified Unmanned Surface Vessel Dynamic Model and Path-Planning of Towed Unmanned Underwater Vehicles [PDF]

open access: yes한국정밀공학회지, 2022
This paper proposes a simplified path-following control method for an Unmanned Surface Vessel (USV) considering towed Unmanned Underwater Vehicles (UUV).
Pyung Mo Ku, Jae Kwan Ryu, Won Hee Lee
doaj   +1 more source

Steering law considering biased loads for control moment gyroscopes

open access: yesMechanical Engineering Journal, 2015
A new steering law of a pyramid configuration of four control moment gyroscopes (CMGs) is proposed to suppress radical motion of gimbals, reduce the gimbal angular displacement and level the biased ones of the four CMGs.
Yasuyuki NANAMORI, Masaki TAKAHASHI
doaj   +1 more source

Hybrid Quasi-Optimal PID-SDRE Quadrotor Control

open access: yesEnergies, 2022
In the paper, a new cascade control system for an autonomous flight of an unmanned aerial vehicle (UAV) based on Proportional–Integral–Derivative (PID) and finite-time State-Dependent Riccati Equation (SDRE) control is proposed.
Wojciech Giernacki   +3 more
doaj   +1 more source

Multi-Layer Adaptive Finite Time Super Twisting Control for Quaternion-Based Quadrotor Formation With Obstacle Avoidance

open access: yesIEEE Access, 2020
This article investigates the trajectory tracking problem of quadrotor formation with collision avoiding. The safety distributed control strategy is introduced for quaternion-based multiple quadrotors formation to avoid collision.
Guowei Zhang   +4 more
doaj   +1 more source

Attitude Control of Two-Wheel Spacecraft Based on Dynamics Model via Hierarchical Linearization

open access: yesSICE Journal of Control, Measurement, and System Integration, 2017
In this paper, we propose an attitude control law for underactuated two-wheel spacecraft under non-zero total angular momentum. Attitude control with non-zero total angular momentum is complicated in the case that the number of reaction wheels equipped ...
Tomohiro Fukaishi   +2 more
doaj   +1 more source

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