Attitude Estimation for a Flexible Spacecraft in an Unstable Spin

Journal of Guidance, Control, and Dynamics - United States
doi 10.2514/2.4853
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

Sliding Mode Attitude Control for Flexible Spacecraft

2014English

Fault-Tolerant Attitude Control for Flexible Spacecraft With Input Saturation

International Robotics & Automation Journal
2017English

Fuzzy Attitude Control of Flexible Multi-Body Spacecraft

2011English

Robust Optimal PID Controller Design for Attitude Stabilization of Flexible Spacecraft

Kybernetika
ControlSystems EngineeringInformation SystemsElectronic EngineeringElectricalTheoretical Computer ScienceArtificial IntelligenceSoftware
2018English

Adaptive Backstepping Attitude Control Law With L2-Gain Performance for Flexible Spacecraft

International Journal of Aerospace Engineering
Aerospace Engineering
2019English

State-Dependent Pseudo-Linear Filters for Spacecraft Attitude and Rate Estimation

2002English

Modeling and Attitude Control of Flexible Spacecraft. An Experimental Study by Using a Single-Axis-Table.

Nippon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C
Mechanics of MaterialsIndustrialMechanical EngineeringManufacturing Engineering
1988English

Terminal Intertial Attitude Control for a Spacecraft

Mehatronika, Avtomatizacia, Upravlenie
2016English

A Robust Optimization Approach for Magnetic Spacecraft Attitude Stabilization

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

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy