Trajectory optimization of a lunar direct landing from halo-orbits body problem. The
descent operation consists of two stages: change in velocity for
descent from orbit
Combined partial regularization and descent method for a generalized primal-dual systemCombined partial regularization and
descent method for a generalized primal-dual system
Neural network software technology trainable on the random search and gradient descent principlesNeural network software technology trainable on the random search and gradient
descent principles
A Logarithmic Barrier Approach Via Majorant Function for Nonlinear Programming
+.
The
descent direction has been calculated using a classical Newton
method, however the step size has
been
Adaptive Conditional Gradient Method adaptive conditional gradient
method with the step length regulation for solving pseudo-convex constrained
Laser beam shaping based on amplitude-phase control of a fiber laser arrayAdamov, E. V.,
Aksenov, Valerii P.,
Atuchin, Victor V.,
Dudorov, V. V.,
Kolosov, V. V.,
Levitsky, M. E. gradient
descent (SPGD)
method is used along with the inversion of a required phase distribution with a
Combined partial regularization and descent method for a generalized primal-dual systemCombined partial regularization and
descent method for a generalized primal-dual system