OPTIMAL PRINCIPLE FOR DYNAMICAL SYSTEM WITH ALTERATIVE ORBITING

Lysenko Alexander
2016 Aviation   unpublished
Lagrange problem with the account of functional limitation at any functional limitations at any moment in a given interval is presented. The required conditions for optimal trajectories of the determinated dynamic system synthesized as space vehicle trajectories have been obtained.
fatcat:ml5qcc4v45hp7gleih2qy7fbbq