000			05104nam a22004937a 4500
001			NM000552
003			AR-HaUTN
005			20240930172040.0
007			ta
008			98020sc. 1 ||||||||||||||000 | spa||
020			_a0471506516
040			_aAR-HaUTN _cAR-HaUTN
100			_aBlakelock, John H. _93063
245			_aAutomatic control of aircraft and missiles _cJohn H. Blakelock
250			_a2nd. ed.
260			_aNew York _bJohn Wiley
300			_axv, 646 p. _bgráficos
500			_aIndice alfabético, al final del libro
504			_aReferencias bibliográficas, al final de cada capítulo
505			_tLongitudinal dynamics : Introduction. The meaning of velocoties in a moving axis system. Development of the equations of motion (Controls locked). Aircraft attitude with respect to the earth. Linearization and separation of the equations of motion. Longitudinal equations of motion. Derivation of equations for the longitudinal stability derivatives. Solution of the longitudinal equations (Stick fixed). Longitudinal transfer function for elevator displacement. Trasient response of the aircraft. Effect of variation of stability derivatives on aircraft performance.
505			_tLongitudinal autopilots : Displacement autopilot. Pitch orientational control system. Acceleration control system. Gilde slope coupler and automatic flare control. Flight path stabilization. Vertical gyro as the basic attitude reference. Gyro stabilized platform as the basic attitude. Effects of nonlinearities
505			_tLateral dynamics : Lateral equations of motion. Derivation of equations for the lateral stability. Derivatives. Solution of lateral esquations (stick fixed). Lateral transfer function for rudder. Displacement. Lateral transfer function for aileron. Displacement. Approximate transfer functions. Transient response of the aircraft. Effect of stability derivative variation
505			_tLateral autopilots : Introduction. Damping of the dutch roll. Methods of obtaining coordination. Discussion of coordination techniques. Yaw orientational control system. Other lateral autopilot configurations. Turn compensation. Automatic lateral beam guidance. Nonlinear effects
505			_tInertial cross-coupling : Introduction. Effects of high roll rates. Determination of the aircraft parameters that affect stability. System for controlling an aircraft subject to inertial cross-coupling. Imprved system for controlling an aircraft subject to inertial cross-coupling
505			_tSel-fadaptive autopilots : Introduction. General philosophy of the self-adaptive control system. Sperry sepf-adaptive control system. Minneapolis-Honeywell self-adaptive control system. Mit model-reference adaptive control system for aircraft. MH-90 adaptive control system. Summary
505			_tMissile control systems : Introduction. Rollstabilization. Control of aerodynamic missiles. transfer function for a ballistic-type missile. Vanguard control system(rigid missile). Alternate missile control system(rigid missile). Summary
505			_tGuidance systems : Introduction. Proportional navigation guidance. Comparison of guidance system performance.. Bank-to turn missile guidance. Short/medium-range BTT missile.
505			_tIntegrated flight / Fire control system : Introduction. Director fire control system. Longitudinal flight control system. Lateral flight control system. Verification of lateral control system analysis. Velocity control system. Movable gun control. Gimbaled tracker desing. Tracking control laws (TCL). Discrete analysis. Simulation resuls.
505			_tMultivariable control systems : Introduction. Multivariable desing without servo dynamics. Multivariable desing with servo dynamics. Multivariable desing of YOCS. Sumary.
505			_tStructural flexibility : Introduction. Lagrange´s equation. Lagrange´s equation apllied to a system of lumped para meters. Mode shapes and frequencies. Normal coordinates. System transfer function, including body bending. The "Tail-WagsDog" Zero. Effects of propellant sloshing. Compensation required for body bending. Summary
505			_tApplication of statistical design principles : Introduction. Random processes. Mean-square error. Autocorrelation function. Cross-correlation function. Power spectral density. Application of statistical desing principles. Additional applications of stastical design principles. Summary
505			_tPilot modeling : Introduction. Crossover model. The paper pilot. Optimal pilot model.
505			_tReview of vector analysis [Appendix A] :
505			_tSome gyroscopic theory [Appendix B]
505			_tBasic servo theory [Appendix C]
505			_tFundamental aerodynamic principles [Appendix D]
505			_tMatrices [Appendix E]
505			_tF94A and F15 longitudinal and lateral aerodynamic data [Appendix F]
505			_tWind axes [Appendix G]
505			_tDigital simulation of transfer functions [Appendix H]
505			_tFire control problem [Appendix I]
505			_tA1 and A4 gunsights [Appendix J]
942			_cBK _2udc
999			_c552 _d552