Simulation results indicate that the closed-form guidance law with robustness is fit to the finite propulsive reentry mission and insensitive to the initial position errors, propulsion direction errors and observation errors.
Simulation results indicate that the closed-form guidance law with robustness is fit to the finite propulsive reentry mission and insensitive to the initial position errors, propulsion direction errors and observation errors.
仿真结果表明，该闭路初制导能够完成有限推力情况下的再入初制导任务，对初始位置误差、推力方向偏差和测量误差不敏感，具有一定的鲁棒性和适应性。