Optimal Trajectory Determination and Mission Design for Asteroid/Deep-Space Exploration via Multibody Gravity Assist Maneuvers

<table class="table-group" id="tab6"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td class="align_left"> </td><td class="align_center">Direct</td><td class="align_center">Single</td><td class="align_center">Double</td><td class="align_center">Triple</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td class="align_left">Total <svg height="8.8423pt" id="M86" style="vertical-align:-0.2064009pt" version="1.1" viewbox="-0.0498162 -8.6359 17.7155 8.8423" width="17.7155pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M600 0V24L339 665L311 657L43 24V0H600ZM497 50H107L303 539L497 50Z" id="g113-133"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="641" vert-adv-y="641" xpluscharwidth="8.333"></glyph.data></g><g transform="matrix(.013,0,0,-0.013,8.327,0)"><path d="M697 650H468L461 623L492 619C539 613 547 605 518 546C481 471 367 264 278 116H276C239 278 197 500 186 567C180 604 185 613 226 619L252 623L260 650H24L17 623C78 617 92 613 108 533L216 -11H247C365 200 515 462 560 529C616 612 624 615 689 623L697 650Z" id="g113-87"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="709" vert-adv-y="709" xpluscharwidth="17.544"></glyph.data></g></svg> [km/sec]</td><td class="align_center">13.452</td><td class="align_center">9.420</td><td class="align_center">10.714</td><td class="align_center">93.611</td></tr><tr><td class="align_left">Orbiter <svg height="8.8423pt" id="M87" style="vertical-align:-0.2064009pt" version="1.1" viewbox="-0.0498162 -8.6359 17.7155 8.8423" width="17.7155pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M600 0V24L339 665L311 657L43 24V0H600ZM497 50H107L303 539L497 50Z" id="g113-133"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="641" vert-adv-y="641" xpluscharwidth="8.333"></glyph.data></g><g transform="matrix(.013,0,0,-0.013,8.327,0)"><path d="M697 650H468L461 623L492 619C539 613 547 605 518 546C481 471 367 264 278 116H276C239 278 197 500 186 567C180 604 185 613 226 619L252 623L260 650H24L17 623C78 617 92 613 108 533L216 -11H247C365 200 515 462 560 529C616 612 624 615 689 623L697 650Z" id="g113-87"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="709" vert-adv-y="709" xpluscharwidth="17.544"></glyph.data></g></svg> [km/sec]</td><td class="align_center">3.823</td><td class="align_center">2.543</td><td class="align_center">3.799</td><td class="align_center">89.866</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mission <svg height="8.8423pt" id="M85" style="vertical-align:-0.2064009pt" version="1.1" viewbox="-0.0498162 -8.6359 17.7155 8.8423" width="17.7155pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M600 0V24L339 665L311 657L43 24V0H600ZM497 50H107L303 539L497 50Z" id="g113-133"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="641" vert-adv-y="641" xpluscharwidth="8.333"></glyph.data></g><g transform="matrix(.013,0,0,-0.013,8.327,0)"><path d="M697 650H468L461 623L492 619C539 613 547 605 518 546C481 471 367 264 278 116H276C239 278 197 500 186 567C180 604 185 613 226 619L252 623L260 650H24L17 623C78 617 92 613 108 533L216 -11H247C365 200 515 462 560 529C616 612 624 615 689 623L697 650Z" id="g113-87"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="709" vert-adv-y="709" xpluscharwidth="17.544"></glyph.data></g></svg> to Hylonome for multiple flyby scenarios.

International Journal of Aerospace Engineering

tab6

Table 6

Table 6: Optimal Trajectory Determination and Mission Design for Asteroid/Deep-Space Exploration via Multibody Gravity Assist Maneuvers 