Khoroshylov Y. Research and accuracy improvement methods for spacecraft attitude control systems

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0408U000018

Thesis Registration Form

0408U000018.pdf

Applicant for

Specialization

  • 05.13.03 - Системи та процеси керування

20-12-2007

Specialized Academic Board

Д.26.205.01

Essay

The proposal under consideration is the method of optimum filtering of stellar sensors data. The method based on these sensors allows to essentially decrease error of spacecraft attitude determination. The paper presents ratios to analyze and estimate precision of attitude determination in the specified direction of elements (ADCS sensors, payload instrumentation, antennas etc.) installed in non-stationary manner on spacecraft.

Read more

Files

Akt 18k-08.jpg

aref.doc

dis.doc

Similar theses

0423U100061

Hrudinina Hanna Serhiivna

Improvement of an autonomous underwater vehicle speed stabilization system

0521U101709

Lytviak Oleksandr M.

Models and methods of analysis of dynamic processes in the automatic control system of a turboshaft gas turbine engine of a helicopter

0421U103122

Aloba Leo Tosin

Group control automation of search-type autonomous underwater vehicles

0421U000086

Aloba Leo Tosin

Group control automation of search-type autonomous underwater vehicles

0521U101109

Holubek Oleksandr V.

Methods and mathematical models of the combined removal of large-sized orbital debris objects