Aircraft Control and Simulation

ISBN-10: 0471371459

ISBN-13: 9780471371458

Edition: 2nd 2004 (Revised)

List price: $160.00 Buy it from $28.26
This item qualifies for FREE shipping

*A minimum purchase of $35 is required. Shipping is provided via FedEx SmartPost® and FedEx Express Saver®. Average delivery time is 1 – 5 business days, but is not guaranteed in that timeframe. Also allow 1 - 2 days for processing. Free shipping is eligible only in the continental United States and excludes Hawaii, Alaska and Puerto Rico. FedEx service marks used by permission."Marketplace" orders are not eligible for free or discounted shipping.

30 day, 100% satisfaction guarantee

If an item you ordered from TextbookRush does not meet your expectations due to an error on our part, simply fill out a return request and then return it by mail within 30 days of ordering it for a full refund of item cost.

Learn more about our returns policy

Description: This second edition covers aerodynamics, the control systems and the mathematics involved in analysing the performance of aircraft not only in the real world but also in computer-simulated flight and gaming. It includes new computer calculations in MatLab, which is commonly used in the industry.

New Starting from $162.05
what's this?
Rush Rewards U
Members Receive:
coins
coins
You have reached 400 XP and carrot coins. That is the daily max!

Study Briefs

Limited time offer: Get the first one free! (?)

All the information you need in one place! Each Study Brief is a summary of one specific subject; facts, figures, and explanations to help you learn faster.

Add to cart
Study Briefs
Italian Grammar Online content $4.95 $1.99
Add to cart
Study Briefs
Italian Grammar Online content $4.95 $1.99
Add to cart
Study Briefs
Portuguese Grammar Online content $4.95 $1.99

Customers also bought

Loading
Loading
Loading
Loading
Loading
Loading
Loading
Loading
Loading
Loading

Book details

List price: $160.00
Edition: 2nd
Copyright year: 2004
Publisher: John Wiley & Sons, Incorporated
Publication date: 10/6/2003
Binding: Hardcover
Pages: 680
Size: 6.75" wide x 9.50" long x 1.50" tall
Weight: 2.684
Language: English

George Vachtsevanos, Phd, is Director of the Intelligent Control Systems Laboratory in the School of Electrical and Computer Engineering at Georgia Institute of Technology, in Atlanta, Georgia.Frank L. Lewis, Phd, is Head of the Advanced Controls, Sensors, and MEMS Group in the Automation and Robotics Research Institute at The University of Texas at Arlington, in Fort Worth, Texas.Michael Roemer, Phd, is Director of Engineering at Impact Technologies, LLC, in Rochester, New York.Andrew Hess is Air System PHM Lead and Development Manager in the Joint Strike Fighter Program Office at Naval Air Systems Command, in Patuxent River, Maryland.Biqing Wu, Phd, works on various topics of active disturbance control and CBM/PHM. She is currently serving as a research engineer at the Georgia Institute of Technology, in Atlanta, Georgia.

List of Tables
List of Examples
Preface
The Kinematics and Dynamics of Aircraft Motion
Introduction
Vector Kinematics
Matrix Analysis of Kinematics
Geodesy, Earth's Gravitation, Terrestrial Navigation
Rigid-Body Dynamics
Summary
Modeling the Aircraft
Introduction
Basic Aerodynamics
Aircraft Forces and Moments
Static Analysis
The Nonlinear Aircraft Model
Linear Models and the Stability Derivatives
Summary
Modeling, Design, and Simulation Tools
Introduction
State-Space Models
Transfer Function Models
Numerical Solution of the State Equations
Aircraft Models for Simulation
Steady-State Flight
Numerical Linearization
Aircraft Dynamic Behavior
Feedback Control
Summary
Aircraft Dynamics and Classical Control Design
Introduction
Aircraft Rigid-Body Modes
The Handling-Qualities Requirements
Stability Augmentation
Control Augmentation Systems
Autopilots
Nonlinear Simulation
Summary
Modern Design Techniques
Introduction
Assignment of Closed-Loop Dynamics
Linear Quadratic Regulator with Output Feedback
Tracking a Command
Modifying the Performance Index
Model-Following Design
Linear Quadratic Design with Full State Feedback
Dynamic Inversion Design
Summary
Robustness and Multivariable Frequency-Domain Techniques
Introduction
Multivariable Frequency-Domain Analysis
Robust Output-Feedback Design
Observers and the Kalman Filter
LQG/Loop-Transfer Recovery
Summary
Digital Control
Introduction
Simulation of Digital Controllers
Discretization of Continuous Controllers
Modified Continuous Design
Implementation Considerations
Summary
F-16 Model
Software
Index
×
Free shipping on orders over $35*

*A minimum purchase of $35 is required. Shipping is provided via FedEx SmartPost® and FedEx Express Saver®. Average delivery time is 1 – 5 business days, but is not guaranteed in that timeframe. Also allow 1 - 2 days for processing. Free shipping is eligible only in the continental United States and excludes Hawaii, Alaska and Puerto Rico. FedEx service marks used by permission."Marketplace" orders are not eligible for free or discounted shipping.

Learn more about the TextbookRush Marketplace.

×