FORMATION FLIGHT SIMULATION SYSTEM

摘要

PURPOSE:To shorten the time required to calculate the position and attitude of a commander plane by performing specific extrapolation processing for a program for calculating the position and attitude of the commander plane. CONSTITUTION:A block 141 solve the fine turbulent motion equation of a stable coordinate system to obtain xa and omega as results. Then a block 142 integrates them to obtain xa and omega as results. A trailing block 143 performs conversion to an inertia coordinate system for the xa according to an attitude matrix to obtain xe as its result. Then a following block 144 calculates the position and attitude according to the xe and omega to obtain xe and L as results, which are applied to the simulation visual field display device of a block 145. Consequently, the time required for the calculation is shortened.