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Fig. 5 The algorithm of guidance law.
Averaging the time-varying coefficients of the optimal guidance law, a suboptimal guidance law is obtained.
The feasibility of the new guidance law is exemplified through computer simulations and the guidance performance is compared with augmented proportional navigation guidance law, sliding mode guidance law and nonsingular terminal sliding mode guidance law.
The optimal guidance law is designed using the proposed method.
It enables guidance law to avoid the latax saturation limits.
The reference roll angle is provided by the guidance law.
Considering the process constraints, the fusion guidance law is obtained.
Simulation results are presented to validate the proposed guidance law.
Simulation results confirm the effectiveness of the proposed guidance law.
Lyapunov stability theorem is used to analyze the guidance law.
By averaging the time-varying coefficients of the optimal guidance law, we obtain a suboptimal guidance law.
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