×







We sell 100% Genuine & New Books only!

Orbital Mechanics And Formation Flying A Digital Control Perspective at Meripustak

Orbital Mechanics And Formation Flying A Digital Control Perspective by Pedro A Capo Lugo, Woodhead

Books from same Author: Pedro A Capo Lugo

Books from same Publisher: Woodhead

Related Category: Author List / Publisher List


  • Price: ₹ 21144.00/- [ 13.00% off ]

    Seller Price: ₹ 18395.00

Estimated Delivery Time : 4-5 Business Days

Sold By: Meripustak      Click for Bulk Order

Free Shipping (for orders above ₹ 499) *T&C apply.

In Stock

We deliver across all postal codes in India

Orders Outside India


Add To Cart


Outside India Order Estimated Delivery Time
7-10 Business Days


  • We Deliver Across 100+ Countries

  • MeriPustak’s Books are 100% New & Original
  • General Information  
    Author(s)Pedro A Capo Lugo
    PublisherWoodhead
    ISBN9780857090546
    Pages350
    BindingHardcover
    LanguageEnglish
    Publish YearJanuary 2011

    Description

    Woodhead Orbital Mechanics And Formation Flying A Digital Control Perspective by Pedro A Capo Lugo

    Aimed at students, faculty and professionals in the aerospace field, this book provides practical information on the development, analysis, and control of a single and/or multiple spacecraft in space. This book is divided into two major sections: single and multiple satellite motion. The first section analyses the orbital mechanics, orbital perturbations, and attitude dynamics of a single satellite around the Earth. Using the knowledge of a single satellite motion, the translation of a group of satellites called formation flying or constellation is explained. Formation flying has been one of the main research topics over the last few years and this book explains different control approaches to control the satellite attitude motion and/or to maintain the constellation together. The control schemes are explained in the discrete domain such that it can be easily implemented on the computer on board the satellite. The key objective of this book is to show the reader the practical and the implementation process in the discrete domain.


    Key Features:-

    • Explains the orbital motion and principal perturbations affecting the satellite
    • Uses the Ares V rocket as an example to explain the attitude motion of a space vehicle
    • Presents the practical approach for different control actuators that can be used in a satellite


    Book Successfully Added To Your Cart