A Comparison of a Predictive Fuzzy Control With an Optimal Control for Automatic Spacecraft Rendezvous.

Journal of the Japan Society for Aeronautical and Space Sciences
doi 10.2322/jjsass1969.39.44
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Japan Society for Aeronautical and Space Sciences

Related search

Rendezvous Docking of a Spacecraft Based on Adaptive Control

Nippon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C
Mechanics of MaterialsIndustrialMechanical EngineeringManufacturing Engineering
2005English

Observer-Based Robust Control for Spacecraft Rendezvous With Thrust Saturation

Abstract and Applied Analysis
Applied MathematicsAnalysis
2014English

Sampled-Data Control of Spacecraft Rendezvous With Discontinuous Lyapunov Approach

Mathematical Problems in Engineering
MathematicsEngineering
2013English

Impulsive Zone Model Predictive Control for Rendezvous Hovering Phases

2019English

Fixed-Time Rendezvous Control of Spacecraft With a Tumbling Target Under Loss of Actuator Effectiveness

IEEE Transactions on Aerospace and Electronic Systems
Electronic EngineeringElectricalAerospace Engineering
2016English

A Hybrid Control Framework for Impulsive Control of Satellite Rendezvous

2016English

Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
2019English

Fuzzy Attitude Control of Flexible Multi-Body Spacecraft

2011English

Deployment Control of a Tethered Satellite System for Rendezvous With a Target

Transactions of the Japan Society for Aeronautical and Space Sciences
SpacePlanetary ScienceAerospace Engineering
2016English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy