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001 ocn769927217
003 OCoLC
005 20160527041038.8
006 m o d
007 cr |n|---|||||
008 120102s2012 njua ob 001 0 eng d
019 778618945|a778813991|a784363620|a794595974|a816879833
020 9781400840601|q(electronic book)
020 1400840600|q(electronic book)
020 9781680159028|q(electronic book)
020 168015902X|q(electronic book)
020 |z0691149216
020 |z9780691149219
020 |z1283379678
020 |z9781283379670
024 8 9786613379672
035 (OCoLC)769927217|z(OCoLC)778618945|z(OCoLC)778813991
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|dCDX|dOCLCQ|dJSTOR|dOCLCQ|dOCLCO|dCOO|dDEBSZ|dIDEBK|dUMI
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049 RIDW
050 4 UG1242.D7
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082 04 623.74/69|a623.7469
090 UG1242.D7
100 1 Beard, Randal W.,|0https://id.loc.gov/authorities/names/
no2008081792|eauthor.
245 10 Small Unmanned Aircraft :|bTheory and Practice /|cRandal
W. Beard, Timothy W. McLain.
264 1 Princeton :|bPrinceton University Press,|c[2012]
300 1 online resource (xiii, 300 pages) :|billustrations
336 text|btxt|2rdacontent
337 computer|bc|2rdamedia
338 online resource|bcr|2rdacarrier
347 text file|2rdaft
500 APPENDIX E: Airframe Parameters.
504 Includes bibliographical references and index.
505 0 Cover; Contents; Preface; 1 Introduction; 1.1 System
Architecture; 1.2 Design Models; 1.3 Design Project; 2
Coordinate Frames; 2.1 Rotation Matrices; 2.2 MAV
Coordinate Frames; 2.3 Airspeed, Wind Speed, and Ground
Speed; 2.4 The Wind Triangle; 2.5 Differentiation of a
Vector; 2.6 Chapter Summary; 2.7 Design Project; 3
Kinematics and Dynamics; 3.1 State Variables; 3.2
Kinematics; 3.3 Rigid-body Dynamics; 3.4 Chapter Summary;
3.5 Design Project; 4 Forces and Moments; 4.1
Gravitational Forces; 4.2 Aerodynamic Forces and Moments;
4.3 Propulsion Forces and Moments; 4.4 Atmospheric
Disturbances.
505 8 4.5 Chapter Summary4.6 Design Project; 5 Linear Design
Models; 5.1 Summary of Nonlinear Equations of Motion; 5.2
Coordinated Turn; 5.3 Trim Conditions; 5.4 Transfer
Function Models; 5.5 Linear State-space Models; 5.6
Reduced-order Modes; 5.7 Chapter Summary; 5.8 Design
Project; 6 Autopilot Design Using Successive Loop Closure;
6.1 Successive Loop Closure; 6.2 Saturation Constraints
and Performance; 6.3 Lateral-directional Autopilot; 6.4
Longitudinal Autopilot; 6.5 Digital Implementation of PID
Loops; 6.6 Chapter Summary; 6.7 Design Project; 7 Sensors
for MAVs; 7.1 Accelerometers.
505 8 7.2 Rate Gyros7.3 Pressure Sensors; 7.4 Digital Compasses;
7.5 Global Positioning System; 7.6 Chapter Summary; 7.7
Design Project; 8 State Estimation; 8.1 Benchmark
Maneuver; 8.2 Low-pass Filters; 8.3 State Estimation by
Inverting the Sensor Model; 8.4 Dynamic-observer Theory;
8.5 Derivation of the Continuous-discrete Kalman Filter;
8.6 Attitude Estimation; 8.7 GPS Smoothing; 8.8 Chapter
Summary; 8.9 Design Project; 9 Design Models for Guidance;
9.1 Autopilot Model; 9.2 Kinematic Model of Controlled
Flight; 9.3 Kinematic Guidance Models; 9.4 Dynamic
Guidance Model; 9.5 Chapter Summary.
505 8 9.6 Design Project10 Straight-line and Orbit Following;
10.1 Straight-line Path Following; 10.2 Orbit Following;
10.3 Chapter Summary; 10.4 Design Project; 11 Path
Manager; 11.1 Transitions Between Waypoints; 11.2 Dubins
Paths; 11.3 Chapter Summary; 11.4 Design Project; 12 Path
Planning; 12.1 Point-to-Point Algorithms; 12.2 Coverage
Algorithms; 12.3 Chapter Summary; 12.4 Design Project; 13
Vision-guided Navigation; 13.1 Gimbal and Camera Frames
and Projective Geometry; 13.2 Gimbal Pointing; 13.3
Geolocation; 13.4 Estimating Target Motion in the Image
Plane; 13.5 Time to Collision.
505 8 13.6 Precision Landing13.7 Chapter Summary; 13.8 Design
Project; APPENDIX A: Nomenclature and Notation; APPENDIX B
: Quaternions; B.1 Quaternion Rotations; B.2 Aircraft
Kinematic and Dynamic Equations; B.3 Conversion Between
Euler Angles and Quaternions; APPENDIX C: Animations in
Simulink; C.1 Handle Graphics in Matlab; C.2 Animation
Example: Inverted Pendulum; C.3 Animation Example:
Spacecraft Using Lines; C.4 Animation Example: Spacecraft
Using Vertices and Faces; APPENDIX D: Modeling in Simulink
Using S-Functions; D.1 Example: Second-order Differential
Equation.
520 Autonomous unmanned air vehicles (UAVs) are critical to
current and future military, civil, and commercial
operations. Despite their importance, no previous textbook
has accessibly introduced UAVs to students in the
engineering, computer, and science disciplines--until now.
Small Unmanned Aircraft provides a concise but
comprehensive description of the key concepts and
technologies underlying the dynamics, control, and
guidance of fixed-wing unmanned aircraft, and enables all
students with an introductory-level background in controls
or robotics to enter this exciting and important area. The
a.
588 Description based on print version record.
590 eBooks on EBSCOhost|bEBSCO eBook Subscription Academic
Collection - North America
650 0 Drone aircraft|xControl systems.|0https://id.loc.gov/
authorities/subjects/sh2002000348
650 0 Drone aircraft|0https://id.loc.gov/authorities/subjects/
sh85039623|xAutomatic control.|0https://id.loc.gov/
authorities/subjects/sh00007651
650 0 Guidance systems (Flight)|0https://id.loc.gov/authorities/
subjects/sh85057711
650 7 Drone aircraft|xControl systems.|2fast|0https://
id.worldcat.org/fast/898350
650 7 Drone aircraft.|2fast|0https://id.worldcat.org/fast/898349
650 7 Automatic control.|2fast|0https://id.worldcat.org/fast/
822702
650 7 Guidance systems (Flight)|2fast|0https://id.worldcat.org/
fast/948964
655 4 Electronic books.
700 1 McLain, Timothy W.,|d1963-|0https://id.loc.gov/authorities
/names/n2011048424|eauthor.
776 08 |iPrint version:|aBeard, Randal W.|tSmall unmanned
aircraft.|dPrinceton, N.J. : Princeton University Press,
©2012|z9780691149219|w(DLC) 2011025926|w(OCoLC)724663112
856 40 |uhttps://rider.idm.oclc.org/login?url=http://
search.ebscohost.com/login.aspx?direct=true&scope=site&
db=nlebk&AN=430164|zOnline eBook. Access restricted to
current Rider University students, faculty, and staff.
856 42 |3Instructions for reading/downloading this eBook|uhttp://
guides.rider.edu/ebooks/ebsco
901 MARCIVE 20231220
948 |d20160607|cEBSCO|tebscoebooksacademic|lridw
994 92|bRID
