並列タイトル等Simulation Program for Rocket Trajectory and Guidance Error Analysis Using Kalman Filter
タイトル（掲載誌）航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
一般注記In this report we present one phase of a study on error analysis of space trajectories,that is to say,how to build an error analysis program based on the modern estimation theory.The proposed method plays an essential role in the post-flight evaluations of the GN＆C system of a space vehicle,and is applicable as well to the mission planning phase.The simulation program thus constructed has the following capabilities:(1) generating any guided trajectories, noisy radar tracking data and IMU outputs(by DATA GENERATOR),and (2)conducting sensitivity analysis and guidance error recovery with regard to almost all guidance parameters in the “consider” option as well as in the “solve-for” option(by TRAJECTORY RE-CONSTRUCTOR).In the appendices,the basic subroutines and some of the application programs for space guidance are presented with the lists for user′s information.
資料番号: NALTM0266000
レポート番号: NAL TM-266
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