针对升力式高超声速飞行器再入滑翔侧向制导问题, 提出了一种考虑禁飞区规避的预测校正制导
方法. 纵向制导采用落点误差预测与指令校正相结合的方式, 不断更新倾侧角的幅值 …

为解决高超声速滑翔式飞行器具有干扰不确定性的再入轨迹优化问题, 提出了一种基于广义正交
多项式方法的随机轨迹优化数值求解方法. 针对随机干扰, 基于广义正交多项式方式对其分布 …

为减小气动参数扰动对火箭助推段的影响, 提高制导精度, 本文将火箭飞行过程中的气动参数
扰动量视为摄动制导中的小扰动量, 对传统摄动方程进行改进. 采用扩展Kalman …

A novel predictor-corrector guidance algorithm is presented for the entry flight with the
terminal altitude constraint. Previous predictor-corrector algorithms focus mainly on the flight …

Reentry trajectory planning and tracking are very important in the design of a hypersonic
glide vehicle. For the problem of poor guidance accuracy in the reentry phase of gliding …

Due to the rapid improvement of the onboard computation capabilities, lots of novel entry
guidance methods have appeared, of which numerical predictor-corrector algorithms have …

Aiming at the problem that the traditional error corridor guidance method has poor
adaptability in lateral guidance of predictor-corrector guidance, an algorithm of reentry …

To solve the defense problem of hypersonic weapon, a coordinated guidance strategy
based on modified proportional navigation guidance law and consensus algorithms for …

For the strong nonlinearity and uncertainty in the ascent guidance problem of air-breathing
hypersonic vehicle, an adaptive ascent guidance scheme based on model predictive static …