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(shè)計(jì)氣動(dòng)力控制系統(tǒng),包括具有角速度反饋的穩(wěn)定內(nèi)回路、跟蹤制導(dǎo)指令的外回路以及各校正環(huán)節(jié)的設(shè)計(jì)。