Two-Phase Optimal Guidance Law considering Impact Angle Constraint with Bearings-Only Measurements

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Case</td><td class="align_center">Impact angle</td><td class="align_center">Handover distance</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">1</td><td class="align_center">−30°</td><td class="align_center">2000 m</td></tr><tr><td class="align_left">2</td><td class="align_center">−60°</td><td class="align_center">1200 m</td></tr><tr><td class="align_left">3</td><td class="align_center">−90°</td><td class="align_center">700 m</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

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Table 2

Table 2: Two-Phase Optimal Guidance Law considering Impact Angle Constraint with Bearings-Only Measurements 