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- Category: Dynamics of. Atmospheric Flight (continued)
- LONGITUDINAL CONTROL
- LINEAR LIFT AND MOMENT
- TOTAL PITCHING MOMENT
- PITCHING MOMENT OF A TAIL
- PITCHING MOMENT OF A BODY AND NACELLES
- PITCH STIFFNESS OF A GENERAL CONFIGURATION
- PITCH STIFFNESS AND POSSIBLE CONFIGURATIONS FOR FLIGHT
- THE BASIC LONGITUDINAL FORCES
- Longitudinal aerodynamic characteristics—part 1
- FURTHER ASSUMPTIONS
- CHOICE OF AXES
- THE SMALL-DISTURBANCE THEORY
- STEADY STATES
- THE FLAT-EARTH APPROXIMATION
- DISCUSSION OF THE SYSTEM OF EQUATIONS
- FORCE AND MOMENT EQUATIONS IN BODY AXES (EULER’S EQUATIONS)
- THE FORCE VECTOR
- FORCE EQUATIONS IN WIND AXES
- THE REMAINDER OF h*
- ROTATING SUBSYSTEM
- THE ANGULAR MOMENTUM
- EQUATIONS OF MOTION OF AN ARBITRARY SYSTEM
- INERTIAL ACCELERATION
- POSITION, VELOCITY, AND ACCELERATION OF THE VEHICLE MASS CENTER
- THE DIRECTION COSINE RATES
- ANGULAR VELOCITIES OF THE SEVERAL REFERENCE FRAMES
- VELOCITY AND ACCELERATION IN AN ARBITRARILY MOVING FRAME
- General equations of unsteady motion
- TRANSFORMATION OF THE DERIVATIVE OF A VECTOR
- THE L MATRIX IN TERMS OF ROTATION ANGLES
- PROPERTIES OF THE L MATRIX
- TRANSFORMATION OF A VECTOR
- THE AERODYNAMIC ANGLES
- DEFINITION OF THE ANGLES
- STABILITY AXES Fs (Osxsyszs)
- BODY-FIXED REFERENCE FRAME FB (BODY AXES, Oxyz)
- ATMOSPHERE-FIXED REFERENCE FRAME, FA (AXES 0AxAyAzA)
- VEHICLE-CARRIED VERTICAL FRAME, Fr (AXES OrYvzr)
- EARTH-FIXED REFERENCE FRAME, FE (EARTH AXES
- DEFINITIONS OF REFERENCE FRAMES USED IN VEHICLE DYNAMICS
- NOTATION
- Reference frames and transformations
- LYAPUNOV STABILITY THEORY
- SINUSOIDAL DESCRIBING FUNCTION
- STEADY-STATE DESCRIBING FUNCTION
- DESCRIBING FUNCTION
- TIME-VARYING AND NONLINEAR SYSTEMS
- . RESPONSE TO A SET OF STATIONARY RANDOM INPUTS
- SUPERPOSITION THEOREM (CONVOLUTION INTEGRAL, DUHAMEL’S INTEGRAL)
- FREQUENCY RESPONSE OF FIRST-ORDER SYSTEM
- EFFECT OF POLES AND ZEROS ON FREQUENCY RESPONSE
- FREQUENCY RESPONSE
- RELATION BETWEEN IMPULSE RESPONSE AND AUTONOMOUS SOLUTION
- INTERPRETATION OF HIGH-ORDER SYSTEM AS A CHAIN
- RESPONSE OF LINEAR/INVARIANT SYSTEMS
- TEST FUNCTIONS FOR A CUBIC
- STABILITY CRITERIA
- CHARACTERISTIC COORDINATES
- CHARACTERISTIC OR NATURAL MODES
- REPEATED ROOTS
- COMPUTATION OF EIGENVALUES AND EIGENVECTORS
- ORTHOGONAL EIGENVECTORS
- EIGENVALUES AND EIGENVECTORS
- AUTONOMOUS LINEAR/INVARJANT SYSTEMS
- TRANSFER FUNCTIONS OF GENERAL LINEAR/INVARIANT SYSTEM
- TRANSFER FUNCTIONS
- EQUILIBRIUM, CONTROL, AND STABILITY
- LINEARITY AND TIME INVARIANCE
- BLOCK DIAGRAM
- EXAMPLE
- System Theory
- MACHINE COMPUTATION
- DISCUSSION OF CONDITION (ii)
- ORDINATE-CROSSING RETURN PERIOD
- MEAN VALUE OF A FUNCTION OF
- PROBABILITY PROPERTIES OF RANDOM VARIABLES
- CORRELATION FUNCTION
- HARMONIC ANALYSIS OF v(t)
- ENSEMBLE AVERAGE
- STATIONARY RANDOM VARIABLE
- RANDOM PROCESS THEORY
- REPEATED ROOTS
- METHODS FOR THE INVERSE TRANSFORMATION
- APPLICATION TO DIFFERENTIAL EQUATIONS
- TRANSFORM OF AN INTEGRAL
- ONE-SIDED LAPLACE TRANSFORM!
- LAPLACE AND FOURIER TRANSFORMS
- VECTOR/MATRIX ALGEBRA
- Analytical tools
- THE TOOLS OF FLIGHT DYNAMICISTS
- Dynamics of Atmospheric Flight
- Category: Events
- In Moscow the helicopter fell to the river about Myakinino
- The broken Ukrainian of Su-25 was entangled in the wires
- The Ukrainian army used again the helicopter with symbolics of the United Nations
- KLM refuses to transport luggage of passengers on flights from Egypt
- Plane crash: to all victims rendered medical aid on a place
- First flight of the new helicopter Mi-38
- Ministry of Transport called a condition of renewal of flights to Egypt
- Mass media: shots on the Ukrainian helicopter was some