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SAAB TN Ae
H Behrbohm The Flat Triangular Wing with Subsonic Leading Edges in Steady Pitch and Roll at Supersonic
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adjoint vectors aircraft and missile aircraft or missiles algorithm altitude variation angle of attack assumed C.L. solutions closed-loop control components constant altitude control histories control variable convergence control corresponding cost value DDP-method decrease depicted in Fig Differential Dynamic Programming differential game problem differential game saddle differential game solution drag coefficient duel formulation evader evasive examples run Figs A4 Figure full throttle game matrix game saddle point gives Hamiltonian hand turn high altitude hmin induced drag initial conditions initial speed iteration kilometers lift coefficient load factor Mach maximum speed Min-Max missdistances missile respectively necessary condition nominal trajectories open-loop control optimal C.L. controls optimal control problem Optimal trajectories optimization method performance criterion Placard limit predicted cost change qmax reference simple pursuit-evasion problems stationary points symmetric initial TF RF RC1-M2 theory throttle setting UNIT variable altitude vehicle weaker missile wingarea zero-drag