Analytical Algorithm for Constructing the Orbital Orientation of a Spacecraft with an Incomplete Measurement of the State Vector Components


Cite item

Full Text

Open Access Open Access
Restricted Access Access granted
Restricted Access Subscription Access

Abstract

The problem of joint synthesis of a modal controller and observer is solved analytically for a sixth-order system that describes the rotational motion of a spacecraft with the available measurements of five components of the state vector. The modeling results that describe the application of the synthesized control and observation laws for the construction of the orbital orientation of a spacecraft are presented in the paper.

About the authors

N. E. Zubov

Bauman Moscow State Technical University

Author for correspondence.
Email: nik.zubov@gmail.com
Russian Federation, Moscow, 105005

A. V. Lapin

Bauman Moscow State Technical University

Email: nik.zubov@gmail.com
Russian Federation, Moscow, 105005

V. N. Ryabchenko

Bauman Moscow State Technical University

Email: nik.zubov@gmail.com
Russian Federation, Moscow, 105005

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2019 Pleiades Publishing, Ltd.