Algorithm for solving optimal open-loop terminal control problem for spacecraft rendezvous with account of constraints on the state

Autor: A. F. Shorikov, A. Yu. Goranov

Publikováno v: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 20, Iss 1, Pp 46-64 (2021)

The paper proposes an algorithm for solving the optimal open-loop terminal control problem of two spacecraft rendezvous with constraints on their states. A system of nonlinear differential equations that describes the dynamics of the active (maneuver

Externí odkaz: https://doaj.org/article/eb1e8ad9ac95408681362ec51d859248