| 摘要 |
PURPOSE: A method for calculating a minimum distance between an outer part separated from an aircraft and other objects is provided to calculate the minimum distance by using points which points comprising a shape of an outer part and points comprising a shape of an adjacent object are faced with each other, thereby reducing the amount of calculation. CONSTITUTION: Points which comprise shapes of an outer part and an adjacent object are read at specific time(S100). A central point of the outer part and the adjacent object is calculated(S200). When inner values are a positive number, a first norm value of the points which comprise the shape of the outer part and the points which comprise the shape of the adjacent object is calculated(S400). [Reference numerals] (AA) Start; (BB) End; (S100) Reading step; (S200) First calculation step; (S300) First discrimination step; (S400) Second discrimination step; (S500) Second discrimination step; (S600) Storage step; (S700) Third determination step; (S800) First determination step; (S900) Second determination step |
