发明名称 GUIDED FLIER
摘要 PROBLEM TO BE SOLVED: To dissolve the problem of a conventional guided flier which cannot get required turn capacity in the turn of a skid-to-turn method, with the form of its airframe being not axially synchronous, such as that it performs the turn in bank-to-turn method and flies, being guided until its meeting with the target, and that it is inferior in responsiveness to that of a skid-to-turn method not requiring to bank since there is necessity to bank the airframe at turn and direct the maximum lift generation plane in the direction of turn in the bank-to-turn method. SOLUTION: This guided flier is one which improves the responsiveness of itself in the vicinity of the target, by switching the turn method from the bank-to-turn method to the skid-to-turn method in the stage where it has come close to the target, after making the form into the airframe form which reduces the L/D ratio of the airframe and does not reduce the turn by the bank-to-turn method.
申请公布号 JP2001141393(A) 申请公布日期 2001.05.25
申请号 JP19990326632 申请日期 1999.11.17
申请人 MITSUBISHI ELECTRIC CORP 发明人 IWAMATSU KAZUYUKI
分类号 F41G7/22;F42B10/64;G05D1/12;(IPC1-7):F41G7/22 主分类号 F41G7/22
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