VFS Website
  • VIEW CART
  • CUSTOMER SUPPORT
  • MY STORE ACCOUNT
  • CONTACT US
  • STORE HOME
  • 5Prime
  • Forum Proceedings
  • Workshops
  • Technical Meetings
  • Vertiflite
  • Books, CDs & Gifts


Unable to log in or get member pricing? Having trouble changing your password?

Please review our Frequently Asked Questions for complete information on these and other common situations.
 

Vertical Flight Library & Store

CHECKOUT

0 Item(s) In Cart Total: $0.00


Hover Flight Control Design for UAS Using Performance-based Disturbance Rejection Requirements

Marcos G. Berrios, Tom Berger, Mark B. Tischler, Ondrej Juhasz, Frank C. Sanders

May 8, 2017

  • Your Path :
  • Home
  • > Hover Flight Control Design for UAS Using Performance-based Disturbance Rejection Requirements

Hover Flight Control Design for UAS Using Performance-based Disturbance Rejection Requirements

  • Presented at Forum 73 - Best Paper for this session
  • 23 pages
  • SKU # : 73-2017-0283
  • December 2018 Paper of the Month.

  • Your Price : $30.00
  • Join or log in to receive the member price of $15.00!


VFS member?
Don't add this to your cart just yet!
Be sure to log in first to receive the member price of $15.00!

 
Add To Cart

Add to Wish List

Reward Value:
(60) Member Points

Hover Flight Control Design for UAS Using Performance-based Disturbance Rejection Requirements

Authors / Details: Marcos G. Berrios, Tom Berger, Mark B. Tischler, Ondrej Juhasz, Frank C. Sanders

Abstract
A key class of UAS are VTOL vehicles, which afford the ability to hover and maneuver in tight spaces; often in windy and turbulent conditions. This paper presents the development and flight testing of optimized control laws for the 3DR IRIS+ quadrotor designed to aggressively hold its position in a hover while subjected to wind gusts and turbulence. Performance-based disturbance rejection requirements, such as attitude/position tracking error in turbulence and maximum position displacement for a 1-cosine gust, are directly incorporated into the flight control design and optimization process. A Control Equivalent Turbulence Input (CETI) was then used to simulate turbulence in flight and the optimized control laws allowed for the quadrotor to hold its position to within 3.5 inches, a factor of 13.5 improvement over the stock position hold controller.

Recently Viewed Items

  • Hover Flight Control Design for UAS Using Performance-based Disturbance Rejection Requirements

    Member Price :
    $15.00
    Your Price :
    $30.00

Popular Products

  • Master Card
  • Visa
  • American Express
  • Customer Support
  • Contact Us
  • Privacy and Security Policies
  • Refund Policies

Copyright © 2022 The Vertical Flight Society. All rights reserved.