## Aerospace Vehicle Flight Control Systems |

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### Contents

Relationships Between Optimal and Conventional Good SystemsA | 1 |

UpSTAGE Missile Flight Control System John L Pearson | 8 |

Wind Gusts0300 ft AltitudeHomogeneous Terrain G B Skelton | 21 |

2 other sections not shown

### Common terms and phrases

aerodynamic Air Force aircraft altitude amplitude angle of attack approximately asymptote capability in left capability in right closed-loop roots closed-loop system coefficient command controlled element gain conventional cost function coupling cross correlations crossover frequency crosswind downwind effect equations f Cq fcoc flight control systems Flight Dynamics flight test Flow Difference Sensor fluidic gust components gust covariance tensor gust energy gust model high-frequency hydraulic systems inputs Kc/s Laplace transform leak-detection level left wing Half-power lifting body linear liquid metal mean wind Navier-Stokes equations negative nonlinear open-loop function operation optimal control optimal cost optimal system P-Q curve parameter performance index phase margin pitch positive-definite ratio Richardson number roll maneuver root locus root square locus servoactuation servovalve shear shown in Fig side gusts spectral stability synthesis techniques temperature tion transfer function UpSTAGE V/STOL valve variable orifice vehicle wing Half-power capability zero