Minimax estimation of space vehicle trajectory by condition of incomplete information
Technical cybernetics. Information technology. Computer facilities
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractThe problem of parametеr identification of the space vehicle trajectory regression model with incomplete apriory information about the pаrameter and noise characteristics is considered. The minimax method of systematic error compensation is suggested. The explicit expressions for the minimax linear estimators in some valuable special cases are presented. The of corresponding numerical tests are considered.