A Convex Approach for Trajectory Optimization of Super-Synchronous-Transfer-Orbit Large Launch Systems with Time-Position Constraints

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Parameters</td><td class="align_center">Deviations</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Semimajor axis, m</td><td class="align_center">1.56</td></tr><tr><td class="align_left">Eccentricity</td><td class="align_center">0.0000001</td></tr><tr><td class="align_left">Inclination, deg</td><td class="align_center">0.0001</td></tr><tr><td class="align_left">Longitude of ascending node, deg</td><td class="align_center">-0.0002</td></tr><tr><td class="align_left">Argument perigee, deg</td><td class="align_center">0.0001</td></tr><tr><td class="align_left"><span class="nowrap"><svg height="11.927pt" id="M194" style="vertical-align:-3.291101pt" version="1.1" viewbox="-0.0498162 -8.6359 11.7401 11.927" width="11.7401pt" 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="M593 650H142L136 622C219 616 224 611 209 531L130 120C114 39 108 34 23 28L17 0H501C518 32 557 130 568 158L540 169C519 132 495 93 469 70C439 43 409 35 332 35C272 35 241 37 225 50C211 61 211 89 222 149L253 320H350C441 320 443 312 441 239H471L510 434H481C455 366 448 358 360 358H260L303 572C311 613 312 615 348 615H431C509 615 522 603 532 581C544 555 546 531 545 491L574 493C583 555 592 631 593 650Z"></path></g><g transform="matrix(.0091,0,0,-0.0091,7.943,3.132)"><path d="M329 433H203L239 587L230 596L147 534L123 433H57L30 395L34 388H115L61 129C37 16 59 -12 85 -12C147 -12 222 58 260 98L241 125C212 95 160 62 144 62C132 62 127 71 138 126L192 386L305 394L329 433Z"></path></g></svg>,</span> s</td><td class="align_center">0.07</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Deviations of terminal orbital elements.</div>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: A Convex Approach for Trajectory Optimization of Super-Synchronous-Transfer-Orbit Large Launch Systems with Time-Position Constraints 