Development of a Full Flight Envelope Helicopter Simulation Using System Identification

著录项

• 来源
  《Journal of the American Helicopter Society》 |2010年第2期|p.022003.1-022003.15|共15页
• 作者

  Lior Zivan; Mark B. Tischler;

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• 作者单位

  Flight Control Systems Department, Engineering Division Israel Aerospace Industries Ben Gurion International Airport, Tel Aviv, Israel;

  Aeroflightdynamics Directorate (AMRDEC) U.S. Army Research, Development and Engineering Command Ames Research Center, Moffett Field, CA;

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• 收录信息
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  A, B, C, D: state-space representation of aircraft dynamics; A_1: lateral input, (+right); B_1: longitudinal input, (+ forward); a_(1s): longitudinal tip-path plane flapping, rad (+ aft); a_x,a_y, a_z: accelerometer signals in body axes, m/s~2; et al;

  机译：A;B;C;D：飞机动力学的状态空间表示;A_1：横向输入;％（+ right）;B_1：纵向输入;％（正向）;a_（1s）：纵向尖端路径平面拍打;rad（+后）;a_x;a_y;a_z：人体轴上的加速度计信号;m / s〜2;等;