What is it about?
The aerodynamic drag effect is incorporated into the optimal impact angle control guidance law. Since the obtained guidance law is closed-form, it can be easily implemented without resorting to numerical methods. Through simulations, it is demonstrated that the proposed guidance law is more effective than the existing methods.
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This page is a summary of: Optimal Impact Angle Control Guidance Law Considering Aerodynamic Drag, Journal of Guidance Control and Dynamics, November 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008234.
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