並列タイトル等General Purpose Flight Simulation Program(FSKP-I) Part 1:Contents of the Program
タイトル（掲載誌）航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-702
一般注記In developing an aircraft, appropriate flight simulation tests are indispensable during the course of the design. The airworthiness of an aircraft is concerned with such main subjects as flight characteristics, including stall at high angle of attack, failure of engines and automatic flight control systems, encounter with strong atmospheric disturbances as well as the design and performance tests of advanced automatic flight control systems. These are design problems caused by large aircraft motion and strong non-linear aerodynamic characteristics, which could only be made clear by simulation tests. The FSPK-I(Flight Simulation Program of Koh-gi-ken)is a simulation program which simulates acculately the above mentioned large non-linear aircraft motion and is intended as an integrated design tool in the development of an aircraft. We have repeatedly used this program since 1977 in the simulation tests for National Aerospace Laboratory’s Quiet-STOL experimental aircraft to demonstrate it’s effectiveness and have looked as well as to the improvement of it’s accuracy and applicability. The FSPK-I has the following characteristics, advantages and limitations. 1)AS operation is based on the fixed point method, the objective aircraft is limited to a medium subsonic aircraft of moderate motion. 2)In the preceding scope, the program has a high general applicability. 3)In the aerodynamic model of the program, the empenage contributions with its non-linearity are independently calculated. 4)The effect of aircraft motion on engine failure can be accurately evaluated by an engine failure conversion coefficient. 5)The program has an automatic trim capability to start the simulation at any flight point. 6)Independent calculation for control response and gust response etc, are possible by cutting off the cockpit signal. 7)A fixed based cockpit is a prerequiste for the program.
資料番号: NALTR0702000
レポート番号: NAL TR-702
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44959&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ