Minimum energy control of a class of electrically driven vehicles
Minimum energy control of class of electrically driven vehicles with application to lunar roving vehicles
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Minimum energy control of class of electrically driven vehicles with application to lunar roving vehicles
Flight comparison of techniques for determining minimum flying speed for large, subsonic jet transport
Approximate analytical solution for minimum impulse transfer between circular orbit and given hyperbolic velocity vector at infinity
Minimum heating flight mode for high lateral range space shuttle reentry based on boundary layer transition criteria
Algorithm for fixed time minimum energy discrete optimal control problems of linear plants with convex constraints imposed on terminal state
Hysteresis effect on cosmic ray modulation and gradient ionization near solar minimum from measurements made near earth with OGO 1 and 3 ion chambers
Suboptimal closed-loop controller design based on quadratic equivalence for linear time varying process with minimum probability of inequality constraints violation
Minimum weight design for symmetrically stiffened cylindrical shells under compression based on linear orthotropic stability theory
Minimum fuel control for discrete time Gaussian processes, applying results to spacecraft midcourse guidance for earth-Mars mission
Continuous and discrete minimum time problems relationships and state space portraits during application of optimal strategies to system
Vlasov equation approximate solution by minimum energy principle, deriving equilibrium equation for stellar gas
Molecular orbital wave functions for water molecule, using minimum set of Slater orbitals
VTOL aircraft stability augmentation system design based on control theory state variable methods, using minimum power levels
Minimum energy feedback control for electrically driven vehicles by dynamic programming
Closed form solution for minimum fuel constant thrust trajectories for vehicle transfer in vacuum between arbitrary boundary conditions
Computer program includes time minimizing function required for propellant constrained minimum time impulsive transfer between coplanar circular orbits or unrestricted orbits. Basic formulation is extended to include inclined circular or inclined elliptic orbits.
Computer program determines minimum shielding necessary for adequate protection of flight hardware, based on component physical size, methods of shielding to be used, and amount of damage which can be sustained without component failure.
Minimum time delay unit for conventional time multiplexed data compression channels