The aerodynamics subsystem is designed employing classical control methodology , including the inner loop which adopt angular rate feedback to stabilizing the attitude , and the outer loop which track the guidance command , and the proper emendation nets are designed for each loop 采用古典控制理論來設計氣動力控制系統,包括具有角速度反饋的穩定內回路、跟蹤制導指令的外回路以及各校正環節的設計。