Combinatory Attitude Determination Method for High Rotational Speed Rigid-Body Aircraft

<div>Projection of the geomagnetic component <svg height="11.8174pt" id="M117" style="vertical-align:-3.1815pt" version="1.1" viewbox="-0.0498162 -8.6359 20.6001 11.8174" width="20.6001pt" 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="M962 650H795L470 145L347 650H176L170 622C268 613 275 606 244 503L190 322C150 188 132 126 118 91C102 50 80 33 18 28L12 0H245L251 28C175 35 170 48 174 93C177 128 191 180 220 284L292 542H294C331 392 383 150 409 4H432L774 555H776L714 137C700 40 694 34 612 28L606 0H868L874 28C793 34 784 37 797 137L849 533C859 612 863 616 956 622L962 650Z"></path></g><g transform="matrix(.0091,0,0,-0.0091,12.22,3.132)"><path d="M870 650H600L593 618C681 609 684 605 669 516L641 367H261L286 516C302 603 313 610 391 618L398 650H132L123 618C214 610 218 606 200 516L127 130C113 46 107 40 25 32L18 0H290L298 32C204 40 200 42 214 130L250 321H631L596 131C580 47 573 39 484 32L475 0H753L762 32C673 39 668 46 685 130L757 516C772 606 778 610 861 618L870 650Z"></path></g></svg> in the lateral direction of coordinate system <i>A</i> and <i>B</i>.</div>

Mathematical Problems in Engineering

fig4

Figure 4

Figure 4: Combinatory Attitude Determination Method for High Rotational Speed Rigid-Body Aircraft 