Naval Postgraduate School
Dudley Knox Library
NPS Dudley Knox Library
View Item 
  •   Calhoun Home
  • Theses and Dissertations
  • 1. Thesis and Dissertation Collection, all items
  • View Item
  •   Calhoun Home
  • Theses and Dissertations
  • 1. Thesis and Dissertation Collection, all items
  • View Item
  • How to search in Calhoun
  • My Accounts
  • Ask a Librarian
JavaScript is disabled for your browser. Some features of this site may not work without it.

Browse

All of CalhounCollectionsThis Collection

My Account

LoginRegister

Statistics

Most Popular ItemsStatistics by CountryMost Popular Authors

Design and implementation of an inertial navigation system for real time flight of an unmanned air vehicle

Thumbnail
Download
Icon95Mar_Kataras.pdf (5.184Mb)
Download Record
Download to EndNote/RefMan (RIS)
Download to BibTex
Author
Kataras, Dimitris Eleftherios
Date
1995-03
Advisor
Kaminer, I.
Shields, M.K.
Metadata
Show full item record
Abstract
Unmanned Air Vehicles present increasing benefits to potential users, with their portability, low cost, and simplicity of operation in any battle theater. Work performed at the Naval Postgraduate School on the ARCHYTAS vehicle converges to totally unattached, autonomous flight in all regimes. Control of this inherently unstable platform is achieved by a Stability Augmentation System, designed to provide flight worthy response to pilot commands from a remote ground station. A critical part of this controller is the navigation system, which furnishes imperative data for the controlling process. This thesis examines the successful design and integration of an Inertial Navigation Sensor Suite with the already existing flight controller for the ARCHYTAS. An Inertial Measurement Unit (IMU) is selected from available systems, and the integration process is presented. The research focuses on system requirements, controller modification, IMU-controller interface procedures, and hardware configuration and installation. A radio frequency communication link that transmits data from the airborne lMU to the ground based flight controller is also developed and tested. Evaluation of the design and implementation is provided through laboratory, hardware-in-the-loop tests.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
URI
http://hdl.handle.net/10945/31573
Collections
  • 1. Thesis and Dissertation Collection, all items

Related items

Showing items related by title, author, creator and subject.

  • Thumbnail

    Development of a nonlinear 6-degree of freedom miniature rotary-wing unmanned aerial vehicle software model and PID flight path controller using Mathworks Simulink simulation environment 

    Miranda, Ricardo E. (Monterey, California: Naval Postgraduate School, 2009-09);
    This paper describes the development of a 6-degree of freedom (6-DOF), nonlinear, miniature rotary-wing unmanned aerial vehicle (RW UAV) simulation environment using MathWorks Simulink simulation software. In addition ...
  • Thumbnail

    Vision guidance controller for an Unmanned Aerial Vehicle 

    Watson, Mark T. (Monterey, California. Naval Postgraduate School, 1998-12);
    The use of Unmanned Aerial Vehicles (UAVs) in modern military operations for reconnaissance and other missions continues to grow. UAV systems using remote control guidance are limited in range and subject to Electronic ...
  • Thumbnail

    Active Control of Adaptive Optics System in a Large Segmented Mirror Telescope 

    Nagashima, M.; Agrawal, B.N. (2012);
    For a large Adaptive Optics (AO) system such as a large Segmented Mirror Telescope (SMT), it is often difficult, although not impossible, to directly apply common Multi-Input Multi-Output (MIMO) controller design methods ...
NPS Dudley Knox LibraryDUDLEY KNOX LIBRARY
Feedback

411 Dyer Rd. Bldg. 339
Monterey, CA 93943
circdesk@nps.edu
(831) 656-2947
DSN 756-2947

    Federal Depository Library      


Start Your Research

Research Guides
Academic Writing
Ask a Librarian
Copyright at NPS
Graduate Writing Center
How to Cite
Library Liaisons
Research Tools
Thesis Processing Office

Find & Download

Databases List
Articles, Books & More
NPS Theses
NPS Faculty Publications: Calhoun
Journal Titles
Course Reserves

Use the Library

My Accounts
Request Article or Book
Borrow, Renew, Return
Tech Help
Remote Access
Workshops & Tours

For Faculty & Researchers
For International Students
For Alumni

Print, Copy, Scan, Fax
Rooms & Study Spaces
Floor Map
Computers & Software
Adapters, Lockers & More

Collections

NPS Archive: Calhoun
Restricted Resources
Special Collections & Archives
Federal Depository
Homeland Security Digital Library

About

Hours
Library Staff
About Us
Special Exhibits
Policies
Our Affiliates
Visit Us

NPS-Licensed Resources—Terms & Conditions
Copyright Notice

Naval Postgraduate School

Naval Postgraduate School
1 University Circle, Monterey, CA 93943
Driving Directions | Campus Map

This is an official U.S. Navy Website |  Please read our Privacy Policy Notice  |  FOIA |  Section 508 |  No FEAR Act |  Whistleblower Protection |  Copyright and Accessibility |  Contact Webmaster

Export search results

The export option will allow you to export the current search results of the entered query to a file. Different formats are available for download. To export the items, click on the button corresponding with the preferred download format.

A logged-in user can export up to 15000 items. If you're not logged in, you can export no more than 500 items.

To select a subset of the search results, click "Selective Export" button and make a selection of the items you want to export. The amount of items that can be exported at once is similarly restricted as the full export.

After making a selection, click one of the export format buttons. The amount of items that will be exported is indicated in the bubble next to export format.