Genetic Programming Method for Satellite System Topology and Parameter Optimization

<div>Flowchart of two-level optimization of satellite system topology and parameter. The component library consists of all component models that can support the satellite system design [<a href="/journals/ijae/2020/6673848/#B14">14</a>, <a href="/journals/ijae/2020/6673848/#B25">25</a>]. <svg height="11.5564pt" id="M16" style="vertical-align:-2.26807pt" version="1.1" viewbox="-0.0498162 -9.28833 33.3478 11.5564" width="33.3478pt" 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="M493 503C489 551 484 614 483 650H43V622C120 616 128 611 128 525V126C128 40 120 34 40 28V0H312V28C221 34 213 40 213 126V307H316C407 307 412 296 424 227H453V420H424C412 355 407 346 316 346H213V584C213 613 216 616 246 616H322C398 616 419 607 436 579C449 559 455 539 464 499L493 503Z"></path></g><g transform="matrix(.013,0,0,-0.013,6.877,0)"><path d="M135 536C164 536 186 560 186 587C186 617 164 639 136 639C109 639 85 617 85 587C85 560 109 536 135 536ZM252 0V26C188 32 181 38 181 106V451C138 433 90 420 39 412V388C99 379 102 374 102 312V106C102 38 95 32 32 26V0H252Z"></path></g><g transform="matrix(.013,0,0,-0.013,10.204,0)"><path d="M298 36L289 62C276 55 253 45 228 45C202 45 169 60 169 141V397H276C289 405 292 426 282 437H169V574L155 576L90 509V437H45L17 408L21 397H90V107C90 28 125 -12 188 -12C198 -12 213 -8 230 1L298 36Z"></path></g><g transform="matrix(.013,0,0,-0.013,14.223,0)"><path d="M300 -147C201 -63 143 98 143 270S200 602 300 686L282 710C136 610 70 450 70 271V270C70 89 136 -72 282 -170L300 -147Z"></path></g><g transform="matrix(.013,0,0,-0.013,18.721,0)"><path d="M771 650H530L519 613L547 609C579 604 589 598 571 571C542 530 498 474 448 416C412 484 388 542 371 585C367 596 369 597 395 605L421 613L429 650H149L139 613C206 606 220 599 245 544L348 313C276 225 182 116 150 86C113 53 93 43 27 37L16 0H264L274 37L257 41C213 51 210 55 234 92S308 192 371 270L453 85C467 54 463 50 420 42L393 37L385 0H699L708 37C633 46 623 52 582 138L468 375C538 455 595 517 642 562C681 599 694 606 761 613L771 650Z"></path></g><g transform="matrix(.013,0,0,-0.013,28.716,0)"><path d="M275 270C275 450 212 609 64 710L45 686C145 604 203 442 203 270S147 -63 45 -147L64 -170C213 -68 275 89 275 270Z"></path></g></svg> is the fitness function.</div>

International Journal of Aerospace Engineering

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Figure 1

Figure 1: Genetic Programming Method for Satellite System Topology and Parameter Optimization 