Flight Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)
Research Unit I, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Flight Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)
Flight Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)
This report provides a comprehensive set of information on the mathematical models necessary to develop a six-degree-of-freedom nonlinear flight simulation code for the design and evaluation of the guidance and control law for D-SEND#2. This paper also elaborates the sonic boom propagation model to evaluate sonic boom measurement condition at the target boom measurement system and provides a list of modeling error data and evaluation criteria for robustness analysis of the guidance and control law using Monte Carlo simulation (MCS).
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
低ソニックブーム設計概念実証フェーズ2（D-SEND#2）飛行シミュレーションモデル
AA1730014000.pdf
(8.28MB)
