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Appendix A The Apollo Spacecraft Control Problem
Appendix B An AirtoAir Missile Control Problem
2 other sections not shown
air-to-air missile angular velocity arithmetic assumed attitude command attitude control attitude error autopilot avsa bending mode canonical form center-of-mass choice coefficients component constant-coefficient continuous stochastic process control computer program control problem control program control signal cost function covariance covariance matrix cut-off Davidon design problem differential equation disturbance estimate ft/sec gain given gradient INIdd initial integral iteration Johansen Joseph and Tou Kalman lateral velocity linear search mean cost mean-square value measurement noise minimize minimum miss-distance missile acceleration nozzle angle nozzle rate operating period optimal design parameters performance plant procedure quadratic cost quantities of interest radians resulting sample instants sample interval sampled-data controller secant method sequence sIhi space representation steer law stochastic controller subroutines synthesis target terminal thrust vector time-varying controller tion trial variables vector vehicle WdOd weighting matrix white noise XiaiVW zero