A maximum principle re-entry study
Mathematical model of maximum principle of Pontryagin used to find point-to-point reentry trajectory of space vehicle
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Mathematical model of maximum principle of Pontryagin used to find point-to-point reentry trajectory of space vehicle
Optimum stage weight distribution in multistage rocket obtained by discrete maximum principle
Huygen principle for analysis of electromagnetic field in moving isotropic homogeneous and linear medium
Approximate ground state wave function used in variational principle for second order energy
Second order energy correction calculated by Hylleraas variation principle with approximate zero order function, shows no relationship to true value
Optimum stage weight distribution in multistage rocket obtained by discrete maximum principle
Stochastic maximum principle with averaged constraint developed for control problems affected by stochastic process
Inadequacy of Corson variational principle as foundation of classical and quantum dynamics
Dynamic programming and Pontryagin maximum principle
Red shift, inertial system rotation, Mach principle, and metric comparisons for gravitation theories
Complementary variational principles in neutron diffusion theory
The Mini-STEP concept was conceived from a desire by NASA to reduce the cost of the Satellite Test of the Equivalence Principle (STEP) experiment below that of the already downsized Quick STEP concept. The goal was for the total cost, including payload, spacecraft, launch vehicle, reserves and operations to be in the $50 million range.
The Mini-STEP idea was conceived from a desire by NASA to reduce the cost of the Satellite Test of the Equivalency Principle (STEP) experiment below that of the already downsized Quick STEP concept. The goal was for the total cost, including launch vehicle and reserves to be in the $50 m range. The Mini-STEP approach was to start with the Quick STEP concept and reduce every component in cost.
The Boltzmann-Ehrenfest principle of adiabatic invariance has been applied to a resonant microwave cavity containing a dielectric sphere.
Li-O2 batteries have traditionally used carbon based electrodes (graphite, buckypaper) as the cathode of choice due to its good electrical conductivity, stability against non-aqueous electrolytes like Dimethyl ether (DME) and ease of handling. But, the carbon cathode also leads to formation of carbonate by-products that increase overpotentials during charging leading to degradation of cathode and reduction of cyclability. In this work, we investigate some of the well-known oxides as cathodes with focus on the interface between the oxide surfaces and the discharge product: Li2O2, in the Li-O2 battery using first principles computations. Our results show that attention must be paid on choosing the appropriate surface of the oxides. We extend the analysis to suggest other possible oxide chemistries that should be investigated as cathodes in Li-O2 batteries.
Principles of invariance in transport theory
Radiative transfer in plane-parallel atmospheres - invariance principles for anisotropic scattering
Cassegrainian principle to ground antennas for space communication