Robust Dynamic Inverse Controller for Spacecraft Model

Keream, Settar S. and Abdalla, Ahmed N. and Ruzlaini, Ghoni and Mohd Razali, Daud and Mashhadany, Youssif Al (2014) Robust Dynamic Inverse Controller for Spacecraft Model. International Journal Of Scientific Research, 3 (5). pp. 113-117. ISSN 2277 - 8179. (Published)

[img] PDF
paper dynamic inverse earspace.pdf - Published Version
Restricted to Repository staff only

Download (385kB) | Request a copy


Typically, the spacecraft model has high uncertainties and the dynamic inverse inner loop controller alone may not achieve acceptable performance. Therefore, a robust outer loop must be added to compensate this inner- loop deficit. In this paper, a robust controller based on dynamic inverse technique for proto type vehicle X-38 model was proposed. The controller contains two loops. The inner loop is dynamic inverse controller which cancels existing system dynamics and replaces them with designer specified response, and the outer loop is a Linear Quadratic Gaussian (LQG) which is used as a robust approach. Several forms of desired dynamic are presented and evaluated in terms of performance and robustness including a proportional dynamics, proportional integral dynamics, flying quality dynamics and ride quality dynamics. The simulation results shows that flying quality and ride quality have been used as a desired dynamics. The ride quality has been proved to be more robust, then the other desired dynamics, against wide range of system parameter variation.

Item Type: Article
Subjects: T Technology > TK Electrical engineering. Electronics Nuclear engineering
Faculty/Division: Faculty of Electrical & Electronic Engineering
Depositing User: PM Dr. Ahmed N Abd Alla
Date Deposited: 23 Feb 2017 05:10
Last Modified: 03 Oct 2018 07:33
Download Statistic: View Download Statistics

Actions (login required)

View Item View Item