DYNAMICS OF FLIGHT: STABILITY AND CONTROL

By A. HINAY

CONTENTS AIRCRAFT EQUATIONS OF MOTION INTRODUCTION COORDINATE AXES SYSTEMS AERODYNAMIC NOMENCLATURE VECTOR TRANSFORMATION RELATIONSHIP AIRCRAFT ORIENTATION AND POSITION AERODYNAMIC FORCES AND MOMENTS EQUATIONS OF MOTION SIMPLI?CATION TECHNIQUES OF DYNAMIC MODELS LINEARIZATION TAYLOR SERIES SMALL-DISTURBANCE THEORY STEADY-STATE EQUATIONS OF MOTION DECOUPLING LINEARIZATION OF FORCES AND MOMENTS STABILITY AND CONTROL DERIVATIVES PROBLEMS REFERENCES TRIM LONGITUDINAL TRIM FUNDAMENTALS AND REQUIREMENTS LONGITUDINAL TRIM ANALYSIS ELEVATOR ANGLE TO TRIM DURING CRUISING FLIGHT ELEVATOR ANGLE TO TRIM DURING CLIMBING FLIGHT DIRECTIONAL TRIM LATERAL TRIM LATERAL-DIRECTIONAL TRIM TRIM TAB LONGITUDINAL STABILITY FUNDAMENTALS DE?NITIONS DYNAMIC STABILITY ANALYSIS OF A DYNAMIC SYSTEM LONGITUDINAL GOVERNING EQUATIONS OF MOTION GOVERNING DIFFERENTIAL EQUATIONS OF MOTION LONGITUDINAL TRANSFER FUNCTIONS LONGITUDINAL STATE SPACE MODEL LONGITUDINAL FORCE AND MOMENT COEF?CIENTS LONGITUDINAL STATIC STABILITY LONGITUDINAL STATIC STABILITY DERIVATIVES NEUTRAL POINT LONGITUDINAL DYNAMIC STABILITY LONGITUDINAL DYNAMIC STABILITY ANALYSIS TECHNIQUE LONGITUDINAL RESPONSE MODES LONGITUDINAL MODES APPROXIMATION AIRCRAFT REACTION TO LONGITUDINAL DISTURBANCES AIRCRAFT REACTION TO DISTURBANCE IN ANGLE OF ATTACK AIRCRAFT REACTION TO DISTURBANCE IN PITCH RATE AIRCRAFT REACTION TO A SUDDEN CHANGE IN ALTITUDE AIRCRAFT REACTION TO DISTURBANCE IN AIRSPEED CONTRIBUTIONS OF AIRCRAFT COMPONENTS TO LONGITUDINAL STABILITY WING CONTRIBUTION HORIZONTAL TAIL CONTRIBUTION VERTICAL TAIL CONTRIBUTION FUSELAGE CONTRIBUTION AIRCRAFT WEIGHT, MOMENT OF INERTIA, AND CENTER OF GRAVITY CONTRIBUTIONS CONTRIBUTIONS OF OTHER COMPONENTS LATERAL-DIRECTIONAL STABILITY LATERAL-DIRECTIONAL GOVERNING EQUATIONS OF MOTION LATERAL-DIRECTIONAL TRANSFER FUNCTIONS LATERAL-DIRECTIONAL STATE SPACE MODEL LATERAL-DIRECTIONAL FORCE AND MOMENTS COEF?CIENTS DIRECTIONAL STATIC STABILITY LATERAL STATIC STABILITY LATERAL-DIRECTIONAL DYNAMIC STABILITY DYNAMIC STABILITY ANALYSIS TECHNIQUE LATERAL-DIRECTIONAL RESPONSE MODES AIRCRAFT REACTION TO LATERAL-DIRECTIONAL DISTURBANCES AIRCRAFT REACTION TO DISTURBANCE IN BANK ANGLE AIRCRAFT REACTION TO DISTURBANCE IN SIDESLIP ANGLE AIRCRAFT REACTION TO DISTURBANCE IN ROLL RATE AIRCRAFT REACTION TO DISTURBANCE IN YAW RATE AIRCRAFT REACTION TO A SUDDEN CHANGE IN HEADING ANGLE CONTRIBUTIONS OF AIRCRAFT COMPONENTS TO LATERAL-DIRECTIONAL STABILITY AIRCRAFT WEIGHT, MOMENT OF INERTIA, AND CENTER OF GRAVITY CONTRIBUTION LONGITUDINAL CONTROL ELEVATOR EFFECTIVENESS TAKEOFF ROTATION CONTROL PURE PITCHING MOTION APPROXIMATION STICK FORCE AND HINGE MOMENT HINGE MOMENT STICK FORCE LATERAL-DIRECTIONAL CONTROL DIRECTIONAL CONTROL DIRECTIONAL TRANSFER FUNCTIONS YAW CONTROL RUDDER EFFECTIVENESS MINIMUM CONTROL SPEED PURE YAWING MOTION APPROXIMATION LATERAL CONTROL GOVERNING EQUATIONS AILERON CONTROL POWER LATERAL TRANSFER FUNCTIONS TURNING FLIGHT LEVEL TURN GOVERNING EQUATIONS COORDINATED TURN TURN CONTROL PHENOMENA ADVERSE YAW AILERON REVERSAL AUTOMATIC FLIGHT CONTROL SYSTEMS COORDINATE AXES SYSTEMS IN ORDER TO FORMULATE THE ?IGHT MOTION AND AIRCRAFT DYNAMICS, WE NEED TO SELECT A COORDI- NATE SYSTEM AS THE REFERENCE (I E , SYSTEM OF COORDINATES OR FRAME OF REFERENCE) COORDINATE