1.National University of Defense Technolgy,changsha,Hunan 410073,China;2.The Science Institute, Air Force Engineering University, Xian, Shaanxi 710051, China 在知网中查找 在百度中查找 在本站中查找
Based on dynamics equation of aircraft flying at high angles of attack, the dynamical characteristics of aircraft flying at pitching on condition of high angles of attack are qualitatively analyzed. The flying stabilities are raised on the basis of various matching parameters, and then the stable field of aircraft can be divided.