Amanote Research

Amanote Research

    RegisterSign In

Synthesizing Relay-Based Spacecraft Attitude Control and Stabilization Ensuring High Quality Without Velocity Sensors

Herald of the Bauman Moscow State Technical University. Series Instrument Engineering
doi 10.18698/0236-3933-2018-3-104-119
Full Text
Open PDF
Abstract

Available in full text

Date

June 1, 2018

Authors
Р.П. СимоньянцП.В. Аверьянов
Publisher

Bauman Moscow State Technical University


Related search

Decentralized Attitude Alignment Control of Spacecraft Within a Formation Without Angular Velocity Measurements

IFAC Proceedings Volumes
2008English

A Robust Optimization Approach for Magnetic Spacecraft Attitude Stabilization

Journal of Optimization Theory and Applications
ControlManagement ScienceApplied MathematicsOptimizationOperations Research
2016English

A Velocity-Free Attitude Tracking Controller for Rigid Spacecraft

2007English

Terminal Intertial Attitude Control for a Spacecraft

Mehatronika, Avtomatizacia, Upravlenie
2016English

Attitude Control Challenges and Solutions for Hayabusa Spacecraft

2006English

Sliding Mode Attitude Control for Flexible Spacecraft

2014English

Robust Optimal PID Controller Design for Attitude Stabilization of Flexible Spacecraft

Kybernetika
ControlSystems EngineeringInformation SystemsElectronic EngineeringElectricalTheoretical Computer ScienceArtificial IntelligenceSoftware
2018English

Fuzzy Attitude Control of Flexible Multi-Body Spacecraft

2011English

Discrete-Time Nonlinear Attitude Tracking Control of Spacecraft

2019English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy