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An integrated autopilot-and-guidance algorithm that is robust to missile's model parametric and dynamic uncertainties is developed, using Higher Order Sliding Mode (HOSM) quasi-continuous control, for an endoatmospheric missile. Unlike in traditional guidance and control solutions that use a nested-loop design, a single loop integrated design of guidance/autopilot is proposed. 6-Degree of Freedom...
An integrated autopilot-and-guidance algorithm that is robust to missile's model parametric and dynamic uncertainties is developed, using Higher Order Sliding Mode (HOSM) quasi-continuous control, for an endoatmospheric missile. Unlike in traditional guidance and control solutions that use a nested-loop design, a single loop integrated design of guidance/autopilot is proposed. 6-Degree of Freedom...
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