摘要
以射程为指标,研究了最优滑翔方案、最大升阻比滑翔方案等方案弹道,给出了滑翔段方案的确定原则;设计了程序转弯下压及高精度定高控制圆弧拉升的下压弹道段方案;针对巡航段的作战需求,重点设计了高精度稳态巡航方案。三自由度弹道的仿真结果表明,各项性能指标均满足飞行任务的要求,从而验证了所设计的方案的合理性。
Choosing the range as the performance index,the optimization gliding,maximum lift-to-drag ratio gliding and equilibrium gliding were studied,and the gliding scheme choosing principle was given.The driving down scheme with program and the arc drawing scheme which can provide high precise height control were developed.To satisfy the request of battle,the high precision steady cruising scheme was designed in the cruising phase.The flight scheme was validated via three degree-of-freedom trajectory simulation,all index requests were satisfied.
出处
《飞行力学》
CSCD
北大核心
2010年第5期51-54,58,共5页
Flight Dynamics
