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Unmanned aircraft design : (Record no. 562284)

000 -LEADER
fixed length control field 08170nam a2200637 i 4500
001 - CONTROL NUMBER
control field 8049434
003 - CONTROL NUMBER IDENTIFIER
control field IEEE
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200413152925.0
006 - FIXED-LENGTH DATA ELEMENTS--ADDITIONAL MATERIAL CHARACTERISTICS
fixed length control field m eo d
007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION
fixed length control field cr cn |||m|||a
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 171003s2017 caua foab 000 0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 9781681731698
Qualifying information ebook
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
Canceled/invalid ISBN 9781681731681
Qualifying information print
024 7# - OTHER STANDARD IDENTIFIER
Standard number or code 10.2200/S00789ED1V01Y201707MEC004
Source of number or code doi
035 ## - SYSTEM CONTROL NUMBER
System control number (CaBNVSL)swl00407815
035 ## - SYSTEM CONTROL NUMBER
System control number (OCoLC)1005264680
040 ## - CATALOGING SOURCE
Original cataloging agency CaBNVSL
Language of cataloging eng
Description conventions rda
Transcribing agency CaBNVSL
Modifying agency CaBNVSL
050 #4 - LIBRARY OF CONGRESS CALL NUMBER
Classification number TL685.35
Item number .S237 2017
082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.13339
Edition number 23
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Sadraey, Mohammad H.,
Relator term author.
245 10 - TITLE STATEMENT
Title Unmanned aircraft design :
Remainder of title a review of fundamentals /
Statement of responsibility, etc. Mohammad H. Sadraey.
264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Place of production, publication, distribution, manufacture [San Rafael, California] :
Name of producer, publisher, distributor, manufacturer Morgan & Claypool,
Date of production, publication, distribution, manufacture, or copyright notice 2017.
300 ## - PHYSICAL DESCRIPTION
Extent 1 PDF (xiv, 193 pages) :
Other physical details illustrations.
336 ## - CONTENT TYPE
Content type term text
Source rdacontent
337 ## - MEDIA TYPE
Media type term electronic
Source isbdmedia
338 ## - CARRIER TYPE
Carrier type term online resource
Source rdacarrier
490 1# - SERIES STATEMENT
Series statement Synthesis lectures on mechanical engineering,
International Standard Serial Number 2573-3176 ;
Volume/sequential designation # 4
538 ## - SYSTEM DETAILS NOTE
System details note Mode of access: World Wide Web.
538 ## - SYSTEM DETAILS NOTE
System details note System requirements: Adobe Acrobat Reader.
500 ## - GENERAL NOTE
General note Part of: Synthesis digital library of engineering and computer science.
504 ## - BIBLIOGRAPHY, ETC. NOTE
Bibliography, etc. note Includes bibliographical references (pages 189-192).
505 0# - FORMATTED CONTENTS NOTE
Formatted contents note Part I -- 1. Design fundamentals -- 1.1 Introduction -- 1.2 UAV classifications -- 1.3 Design project planning -- 1.4 Decision making -- 1.5 Design criteria, objectives, and priorities -- 1.6 Feasibility analysis -- 1.7 Design groups -- 1.8 Design process -- 1.9 Systems engineering approach -- 1.10 Conceptual design -- 1.11 Preliminary design -- 1.12 Detail design -- 1.13 Design review, evaluation, and feedback -- 1.14 Questions -- 2. Design disciplines -- 2.1 Introduction -- 2.2 Aerodynamic design -- 2.3 Structural design -- 2.4 Propulsion system design -- 2.5 Landing gear design -- 2.6 Mechanical/power transmission systems design -- 2.7 Control surfaces design -- 2.8 Questions --
505 8# - FORMATTED CONTENTS NOTE
Formatted contents note Part II. -- 3. Fundamentals of autopilot -- 3.1 Introduction -- 3.2 Primary subsystems of an autopilot -- 3.3 Dynamic modeling -- 3.4 UAV dynamics -- 3.5 Aerodynamic forces and moments -- 3.6 Stability and control derivatives -- 3.7 Transfer function -- 3.8 State-space model -- 3.9 Linearization -- 3.10 Autopilot design process -- 3.11 Questions -- 4. Control system design -- 4.1 Introduction -- 4.2 Fundamentals of control systems -- 4.3 UAV control architecture -- 4.3.1 Control categories -- 4.3.2 Cruise control -- 4.4 Flight control requirements -- 4.4.1 Longitudinal control requirements -- 4.4.2 Roll control requirements -- 4.4.3 Directional control requirements -- 4.5 PID controller -- 4.6 Optimal control-linear quadratic regulator (LQR) -- 4.7 Robust control -- 4.8 Digital control -- 4.9 Stability augmentation -- 4.10 Autonomy -- 4.10.1 Classification -- 4.10.2 Detect (I.E., sense)-and-avoid -- 4.10.3 Automated recovery -- 4.10.4 Fault monitoring -- 4.10.5 Intelligent flight planning -- 4.10.6 Manned-unmanned teaming -- 4.11 Control system design process -- 4.12 Questions -- 4.13 Problems -- 5. Navigation system design -- 5.1 Introduction -- 5.2 Coordinate systems -- 5.3 Inertial navigation system -- 5.4 Global positioning system -- 5.5 Position fixing navigation -- 5.5.1 Map reading -- 5.5.2 Celestial navigation -- 5.6 Inertial navigation sensors -- 5.6.1 Accelerometer -- 5.6.2 Gyroscope -- 5.6.3 Airspeed sensor -- 5.6.4 Altitude sensor -- 5.7 Design considerations -- 5.8 Questions -- 6. Guidance system design -- 6.1 Introduction -- 6.2 Elements of guidance system -- 6.3 Guidance laws -- 6.4 Line-of-sight guidance law -- 6.5 Formation flight -- 6.6 Proportional navigation guidance law -- 6.7 Pursuit guidance law -- 6.8 Waypoint guidance -- 6.9 Seeker -- 6.10 Questions -- 7. Microcontroller -- 7.1 Introduction -- 7.2 Basic fundamentals -- 7.3 Modules/components -- 7.4 Flight software -- 7.4.1 Software development -- 7.4.2 Operating system -- 7.4.3 Management software -- 7.4.4 Microcontroller programing -- 7.4.5 Software integration -- 7.4.6 C language -- 7.4.7 Compiler -- 7.4.8 ArduPilot -- 7.4.9 Debugging -- 7.4.10 Design procedure -- 7.5 Questions --
505 8# - FORMATTED CONTENTS NOTE
Formatted contents note Part III -- 8. Ground control station -- 8.1 Introduction -- 8.2 GCS subsystems -- 8.3 Human operator in ground station -- 8.4 Types of ground stations -- 8.4.1 Handheld controller -- 8.4.2 Portable GCS -- 8.4.3 Mobile truck -- 8.4.4 Central command station -- 8.5 Communication system -- 8.6 Design considerations -- 8.7 Questions -- 9. Launch and recovery systems -- 9.1 Introduction -- 9.2 Fundamentals of launch -- 9.3 Launcher equipment -- 9.4 Recovery techniques -- 9.5 Recovery fundamentals -- 9.5.1 Parachute -- 9.5.2 Impact recovery -- 9.6 Air launch -- 9.7 Hand launch -- 9.8 Launch and recovery systems design -- 9.9 Questions -- 9.10 Problems -- 10. Payloads selection/design -- 10.1 Introduction -- 10.2 Payload definition -- 10.3 Cargo or freight payload -- 10.4 Reconnaissance/surveillance payload -- 10.4.1 Camera -- 10.4.2 Radar -- 10.5 Scientific payloads -- 10.6 Military payload (weapon) -- 10.7 Payload installation -- 10.7.1 Payload location -- 10.7.2 Payload aerodynamics -- 10.7.3 Payload-structure integration -- 10.7.4 Payload stabilization -- 10.8 Payload control and management -- 10.9 Payload selection/design considerations -- 10.10 Questions -- 10.11 Problems --
505 8# - FORMATTED CONTENTS NOTE
Formatted contents note Bibliography -- Author biography.
506 ## - RESTRICTIONS ON ACCESS NOTE
Terms governing access Abstract freely available; full-text restricted to subscribers or individual document purchasers.
510 0# - CITATION/REFERENCES NOTE
Name of source Compendex
510 0# - CITATION/REFERENCES NOTE
Name of source INSPEC
510 0# - CITATION/REFERENCES NOTE
Name of source Google scholar
510 0# - CITATION/REFERENCES NOTE
Name of source Google book search
520 3# - SUMMARY, ETC.
Summary, etc. This book provides fundamental principles, design procedures, and design tools for unmanned aerial vehicles (UAVs) with three sections focusing on vehicle design, autopilot design, and ground system design. The design of manned aircraft and the design of UAVs have some similarities and some differences. They include the design process, constraints (e.g., g-load, pressurization), and UAV main components (autopilot, ground station, communication, sensors, and payload). A UAV designer must be aware of the latest UAV developments; current technologies; know lessons learned from past failures; and they should appreciate the breadth of UAV design options. The contribution of unmanned aircraft continues to expand every day and over 20 countries are developing and employing UAVs for both military and scientific purposes. A UAV system is much more than a reusable air vehicle or vehicles. UAVs are air vehicles, they fly like airplanes and operate in an airplane environment. They are designed like air vehicles; they have to meet flight critical air vehicle requirements. A designer needs to know how to integrate complex, multi-disciplinary systems, and to understand the environment, the requirements and the design challenges and this book is an excellent overview of the fundamentals from an engineering perspective. This book is meant to meet the needs of newcomers into the world of UAVs. The materials are intended to provide enough information in each area and illustrate how they all play together to support the design of a complete UAV. Therefore, this book can be used both as a reference for engineers entering the field or as a supplementary text for a UAV design course to provide system-level context for each specialized topic.
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Also available in print.
588 ## - SOURCE OF DESCRIPTION NOTE
Source of description note Title from PDF title page (viewed on October 3, 2017).
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Drone aircraft
General subdivision Design and construction.
653 ## - INDEX TERM--UNCONTROLLED
Uncontrolled term unmanned aerial vehicles
653 ## - INDEX TERM--UNCONTROLLED
Uncontrolled term design
653 ## - INDEX TERM--UNCONTROLLED
Uncontrolled term automatic flight control system
653 ## - INDEX TERM--UNCONTROLLED
Uncontrolled term autopilot
653 ## - INDEX TERM--UNCONTROLLED
Uncontrolled term drone
653 ## - INDEX TERM--UNCONTROLLED
Uncontrolled term remotely piloted vehicle
655 #0 - INDEX TERM--GENRE/FORM
Genre/form data or focus term Electronic books.
776 08 - ADDITIONAL PHYSICAL FORM ENTRY
Relationship information Print version:
International Standard Book Number 9781681731681
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
Uniform title Synthesis digital library of engineering and computer science.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
Uniform title Synthesis lectures on mechanical engineering ;
Volume/sequential designation # 4.
International Standard Serial Number 2573-3176
856 42 - ELECTRONIC LOCATION AND ACCESS
Materials specified Abstract with links to resource
Uniform Resource Identifier http://ieeexplore.ieee.org/servlet/opac?bknumber=8049434
Holdings
Withdrawn status Lost status Damaged status Not for loan Permanent Location Current Location Date acquired Barcode Date last seen Price effective from Koha item type
        PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2020-04-13 EBKE784 2020-04-13 2020-04-13 E books

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