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Flight Mechanics Modeling and Analysis [Hardback]

(National Aerospace Laboratories (CSIR-NAL), India), (CSIR-NAL, India)
  • Formāts: Hardback, 436 pages, height x width: 234x156 mm, weight: 861 g, 54 Tables, black and white; 158 Illustrations, black and white
  • Izdošanas datums: 20-Aug-2008
  • Izdevniecība: CRC Press Inc
  • ISBN-10: 1420067532
  • ISBN-13: 9781420067538
Citas grāmatas par šo tēmu:
Flight Mechanics Modeling and AnalysisPalielināt
  • Formāts: Hardback, 436 pages, height x width: 234x156 mm, weight: 861 g, 54 Tables, black and white; 158 Illustrations, black and white
  • Izdošanas datums: 20-Aug-2008
  • Izdevniecība: CRC Press Inc
  • ISBN-10: 1420067532
  • ISBN-13: 9781420067538
Citas grāmatas par šo tēmu:
Permanent link: https://www.kriso.lv/db/9781420067538.html
Keywords:
Aerospace engineers at the National Aeronautical Laboratory in Bangalore Raol (retired) and Singh discuss techniques that have become very important in the design, development, analysis, and evaluation of aerospace vehicles, especially in fly-by-wire aircraft development programs. They illustrate several concepts and methods of flight mechanics as applied to system identification, parameters estimation, simulation, and handling quality evaluations. Annotation ©2008 Book News, Inc., Portland, OR (booknews.com)
Preface xv
Acknowledgments xvii
Authors xix
Introduction
1(10)
ANNs in Control
4(1)
FL/S in Control
5(1)
Evaluation of Aircraft Control-Pilot Interactions
6(1)
Chapter Highlights
7(4)
References
9(2)
Mathematical Model Building
11(42)
Introduction
11(4)
Mathematical Model Structures
15(22)
TF Models
16(1)
Continuous-Time Model
17(5)
Discret-Time Model
22(1)
Delta Form TF
23(3)
State-Space Models
26(1)
State-Space Representations
26(7)
General Model
33(1)
Time-Series Models
34(3)
Models for Noise/Error Processes
37(1)
Continuous-Time/Discrete-Time White/Correlated Noise Processes
37(1)
ANN Modeling
38(7)
Feed Forward Neural Networks
42(1)
A Training Algorithm for FFNN
42(2)
Recurrent Neural Networks
44(1)
FL-Based Modeling
45(8)
Additive Fuzzy System
46(4)
Epilogue
50(1)
Exercises
50(1)
References
51(2)
Equations of Motion
53(30)
Introduction
53(1)
Rigid Body EOM
54(6)
Resolution of Inertial Forces and Moments
60(2)
Resolution of Aerodynamics, Gravity Forces, and Thrust Forces
62(5)
Complete Sets of EOM
67(4)
Rectangular Form
68(1)
Polar Form
69(2)
Missile Dynamic Equations
71(1)
Rotorcraft Dynamics
72(11)
Momentum Theory
74(2)
Blade-Element Theory
76(1)
Rotorcraft Modeling Formulations
76(2)
Limitations of Rigid Body Model
78(1)
Epilogue
79(1)
Exercises
79(1)
References
80(3)
Aerodynamic Derivatives and Modeling
83(38)
Introduction
83(1)
Basic Aerodynamic Forces and Moments
84(2)
Aerodynamic Parameters
86(21)
Definition of Aerodynamic Derivatives
87(3)
Longitudinal Derivatives
90(10)
Lateral-Directional Derivatives
100(6)
Compound Lateral-Directional Derivatives
106(1)
Missile Aerodynamic Derivatives
107(4)
Longitudinal Derivatives
109(1)
Lateral-Directional Derivatives
109(1)
Roll Derivatives
109(1)
Yaw Derivatives
110(1)
Rotorcraft Aerodynamic Derivatives
111(2)
Role of Derivatives in Aircraft Design Cycle and Flight Control Law Development
113(3)
Aircraft Aerodynamic Models
116(5)
Epilogue
118(1)
Exercises
118(1)
References
119(2)
Simplification of Equations of Motion and Transfer-Function Analysis
121(38)
Introduction
121(1)
Strategies for Simplification
122(3)
Choice of Coordinate Systems
122(1)
Linerization of Model Equations
123(1)
Simplification Using Measured Data
124(1)
Longitudinal Models and Modes
125(11)
Short Period Mode
128(5)
Phugoid
133(3)
Lateral-Directional Models and Modes
136(6)
DR Mode
139(1)
Spiral Mode
139(1)
Roll Mode
140(2)
Missile Aerodynamic Transfer Functions
142(3)
Rotorcraft Linear Modeling
145(5)
Rotor Plus Body Models
146(1)
Stability Dervative Models
147(1)
Rotor-Response Decomposition Models
148(1)
Evaluation/Validation of Linear Flight Dynamics Models
149(1)
UAV Dynamics
150(1)
MAV Dynamics
151(2)
Lighter-than-Air Vehicle/BLIMP Dynamics
153(6)
Epilogue
154(1)
Exercises
155(1)
References
156(3)
Simulation of Flight Dynamics
159(34)
Introduction
159(4)
Aircraft Subsystems Data/Models
163(8)
Aero Database
164(1)
Mass, Inertia, and Center of Gravity Characteristics
164(1)
Instrumentation System
165(1)
Interial Navigation System
165(1)
Flight Management System
165(1)
Actuator Models
166(1)
Engine Model
167(1)
Landing Gear
168(1)
Control Loading and Sound Simulation
168(1)
Motion Cues
169(1)
Turbulence and Gust Models
170(1)
Sensor Modeling
170(1)
Flight Dynamics
171(1)
Steady-State Flight and Trim Conditions
171(7)
Rate of Climb and Turn Coordination Flights
174(2)
Computation of Linear Models for Control Law Design
176(2)
Six DOF Simulation and Validation
178(6)
Flight Simulation Model Validation for a Rotorcraft
180(1)
Flight Simulation Model Validation Using the Concept of Coefficient Matching
181(2)
Flight Simulation Model Validation Using Direct Update
183(1)
PC MATLAB®/SIMULINK®-Based Simulation
184(9)
Epilogue
188(1)
Exercises
189(1)
References
190(3)
Flight Test Maneuvers and Database Management
193(36)
Introduction
193(1)
Planning of Flight Test Maneuvers
194(4)
Flight Test Evaluation of a Transport Aircraft
196(1)
Takeoff and Landing Tasks
196(1)
Approach and Landing Task
196(1)
Takeoff Task
197(1)
Other Maneuvers
198(1)
Specific Flight Test Data Generation and Analaysis Aspects
198(4)
Longitudinal Axis Data Generation
199(2)
LD Data Generation
201(1)
Quality of Flight Test Maneuvers
202(1)
Input Signals for Exciting Maneuvers
202(2)
Design Consideration for Input Signals
202(2)
Specific Input Types
204(1)
Specific Maneuvers for Aerodynamic Modeling
204(7)
Small Amplitude Maneuvers
204(1)
Longitudinal Short-Period Maneuver
205(1)
Phugoid Maneuver
205(1)
Thrust Input Maneuver
205(1)
Flaps Input Maneuver
205(1)
LD Maneuvers
206(1)
Aileron Input Roll Maneuver
207(1)
Rudder Input Maneuver
208(1)
DR Maneuver
208(1)
Steady heading Sideslip Maneuver
208(1)
Large Amplitude Maneuvers
208(3)
Specific Dynamic Maneuvers for Determination of Drage Polars
211(6)
Roller Coaster (Pullup/Pushover) Maneuver
213(1)
SD Maneuver
213(1)
Acceleration and Deceleration Maneuver
213(1)
WUT Maneuver
214(3)
Specific Maneuvers for Rotorcaft
217(2)
Flight Test Database Management
219(10)
Basic Requirements
220(1)
Selection and Classification of Flight Data
220(1)
Classification Based on Type of Maneuvers
220(1)
Classification Based on Flight Conditions
221(1)
Classification Based on Aircraft Configuration
221(1)
Data Storage and Organization
221(1)
Flight Test Database in Oracle
221(4)
Brief Description of a Typical Program
225(1)
Transactions
225(1)
Graphs/Reports
225(1)
User Maintenance
226(1)
Epilogue
226(1)
Exercises
226(2)
References
228(1)
Reconfiguration and Fuzzy Control Analysis
229(34)
Introduction
229(1)
Requirements of Flight Control
229(4)
Stability/control Augmentation Strategies
233(3)
Performance Requrements and Criteria
236(1)
Procedure for the Design and Evaluation of Control Laws
236(2)
Fuzzy Logic Control
238(8)
Fault Detection, Identification, and Isolation
246(1)
Models for Faults
246(1)
Aircraft Reconfigurable/Restructurable Control System
247(16)
Sensor Fault Detection Scheme
250(3)
Actuator Fault Detection Scheme
253(1)
Reconfiguration Concept
254(2)
Non-Model-Based Approach
256(2)
Epilogue
258(1)
Exercises
259(1)
References
260(3)
System Identification and Parameter Estimation
263(60)
Introduction
263(3)
System Identification
266(6)
Time-Series/Regression Model Identification
266(2)
Comparison of Several Model Order Criteria
268(3)
Transfer Function Models from Real-Flight Data
271(1)
Expert Systems for System Identification
272(1)
Aircraft Parameter Estimation
272(11)
Maneuvers, Measurements, and Mathematical Models
273(1)
Parameter-Estimation Methods
274(1)
Equation Error Method
274(1)
Maximum Likelihood/OEM
275(4)
Filtering Methods
279(3)
Parameter-Estimation Approaches for Inherently Unstable/Augmented Aircraft
282(1)
Determination of Stability and Control Derivatives from Flight Data---Case Studies
283(9)
Fighter Aircraft FA1
284(1)
Fighter Aircraft FA2
285(1)
Basic and Modified Transport Aircraft
285(2)
Trainer Aircraft
287(1)
Light Canard Research Aircraft
288(1)
Helicopter
288(2)
AGARD Standard Model
290(1)
Dynamic Wind-Tunnel Experiments
290(1)
Iron Bird Results
291(1)
Approaches for Determination of Drag Polars from Flight Data
292(2)
Model-Based Approach for Determination of Drag Polar
293(1)
Non-Model-Based Approach for Drag Polar Determination
293(1)
Analysis of Large Amplitude Maneuver Data
294(2)
Global Nonlinear Analytical Modeling
296(2)
ANN-Based Parameter Estimation
298(5)
FFNN Scheme
299(1)
RNN for Parameter Estimation
300(3)
Fuzzy Logic-Based Methods for Estimation
303(8)
ANFIS for Parameter Estimation
303(2)
Fuzzy Kalman Filter for State Estimation
305(4)
Tracking of Maneuvering Target
309(2)
Derivative-Free Kalman Filter for State Estimation
311(12)
Epilogue
317(1)
Exercises
317(2)
References
319(4)
Handling Qualities Analysis
323(30)
Introduction
323(1)
Pilot Opinion Rating
323(1)
Human Operator Modeling
324(4)
Motion Plus Visual and Only Visual Cue Experiments
325(3)
Handling Qualities Criteria
328(9)
Longitudinal HQ Criteria
329(1)
Lower-Order Equivalent TF
329(1)
Control Anticipation Parameter
329(2)
Bandwidth Criterion
331(1)
Neal-Smith Criterion
331(1)
Closed Loop Criterion
332(1)
Pitch Rate Response
332(1)
C* Criterion
332(1)
Gibson's Criteria
333(1)
Lateral-Directional HQ Criteria
334(1)
Lower-Order Equivalent TF
334(1)
Roll Angle-Sideslip Mode Ratio
334(1)
LD Modes
334(1)
Roll Rate and Bank Angle Oscillations
335(1)
Roll Performance
336(1)
Sideslip Excursions
337(1)
Evaluation of HQ Criteria
337(6)
HQ for Large Transport Aircraft
337(1)
Rotorcraft Handling Qualities
338(2)
Handling Qualities Analysis Tool
340(1)
Hover and Low-Speed Requirements (HLSR)---Pitch Axis Response Criteria
341(1)
HLSR---Roll Axis Response Criteria
341(2)
HLSR---Yaw Axis Response Criteria
343(1)
HLSR---Heave Axis Response Criteria
343(1)
HQ Aspects for Unmanned Aerial Vehicles
343(2)
Pilot-Aircraft Interactions
345(3)
Longitudinal PIO Criteria
345(1)
Ralph-Smith Criterion
346(1)
Smith-Geddes Criterion
346(1)
Phase Rate Criterion
346(1)
Loop Separation Parameter
347(1)
Neal-Smith Time-Domain Criterion
347(1)
Bandwidth PIO Criterion
347(1)
Lateral PIO Criteria
347(1)
Ralph-Smith
348(1)
Phase Rate
348(1)
Model Order Reduction for Evaluations of HQ
348(5)
Epilogue
349(1)
Exercises
349(1)
References
350(3)
Appendix A: Aerodynamics and Related Concepts 353(30)
Appendix B: Statistics and Probability 383(8)
Appendix C: Signal and Systems Concepts 391(16)
Bibliography 407(2)
Index 409
Jitendra R. Raol, Jatinder Singh