PX4 Firmware
PX4 Autopilot Software http://px4.io
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Variables | |
float | t3 = ve-vwe |
float | t4 = q0*q0 |
float | t5 = q1*q1 |
float | t6 = q2*q2 |
float | t7 = q3*q3 |
float | t8 = vd-vwd |
float | t9 = q0*q1*2.0f |
float | t10 = q2*q3*2.0f |
float | t11 = vn-vwn |
float | t13 = q0*q2*2.0f |
float | t14 = q1*q3*2.0f |
float | t18 = t4-t5-t6+t7 |
float | t19 = t8*t18 |
float | t20 = t9-t10 |
float | t21 = t3*t20 |
float | t22 = t13+t14 |
float | t23 = t11*t22 |
float | t2 = t19-t21+t23 |
float | t15 = q0*q3*2.0f |
float | t16 = q1*q2*2.0f |
float | t24 = t9+t10 |
float | t25 = t4-t5+t6-t7 |
float | t26 = t3*t25 |
float | t27 = t8*t24 |
float | t28 = t15-t16 |
float | t29 = t11*t28 |
float | t12 = t26+t27-t29 |
float | t30 = t13-t14 |
float | t31 = t4+t5-t6-t7 |
float | t32 = t11*t31 |
float | t33 = t8*t30 |
float | t34 = t15+t16 |
float | t35 = t3*t34 |
float | t17 = t32-t33+t35 |
float | t44 = t2*t18*2.0f |
float | t45 = t12*t24*2.0f |
float | t46 = t17*t30*2.0f |
float | t36 = t44+t45-t46 |
float | t37 = t2*t2 |
float | t38 = t12*t12 |
float | t39 = t17*t17 |
float | t40 = t37+t38+t39 |
float | t41 = 1.0f/t40 |
float | t48 = t12*t25*2.0f |
float | t49 = t2*t20*2.0f |
float | t50 = t17*t34*2.0f |
float | t42 = t48-t49+t50 |
float | t52 = t17*t31*2.0f |
float | t53 = t2*t22*2.0f |
float | t54 = t12*t28*2.0f |
float | t43 = t52+t53-t54 |
float | t47 = t36*t36 |
float | t51 = t42*t42 |
float | t55 = t43*t43 |
float | t57 = 1.0f/(t17*t17) |
float | t58 = 1.0f/t17 |
float | t63 = t18*t58 |
float | t64 = t2*t30*t57 |
float | t56 = t63+t64 |
float | t66 = t22*t58 |
float | t67 = t2*t31*t57 |
float | t59 = t66-t67 |
float | t60 = t37*t57 |
float | t61 = t60+1.0f |
float | t62 = 1.0f/(t61*t61) |
float | t65 = t56*t56 |
float | t68 = t59*t59 |
float | t70 = t20*t58 |
float | t71 = t2*t34*t57 |
float | t69 = t70+t71 |
float | t72 = t69*t69 |
float | t78 = t25*t58 |
float | t79 = t12*t34*t57 |
float | t73 = t78-t79 |
float | t81 = t28*t58 |
float | t82 = t12*t31*t57 |
float | t74 = t81+t82 |
float | t75 = t38*t57 |
float | t76 = t75+1.0f |
float | t77 = 1.0f/(t76*t76) |
float | t80 = t73*t73 |
float | t83 = t74*t74 |
float | t85 = t24*t58 |
float | t86 = t12*t30*t57 |
float | t84 = t85+t86 |
float | t87 = t84*t84 |
float | tas_var = t41*t47*vd_var*0.25f+t41*t51*ve_var*0.25f+t41*t55*vn_var*0.25f+t41*t47*vwd_var*0.25f+t41*t51*vwe_var*0.25f+t41*t55*vwn_var*0.25f |
float | aoa_var = t62*t65*vd_var+t62*t72*ve_var+t62*t68*vn_var+t62*t65*vwd_var+t62*t72*vwe_var+t62*t68*vwn_var |
float | aos_var = t77*t87*vd_var+t77*t80*ve_var+t77*t83*vn_var+t77*t87*vwd_var+t77*t80*vwe_var+t77*t83*vwn_var |
float aoa_var = t62*t65*vd_var+t62*t72*ve_var+t62*t68*vn_var+t62*t65*vwd_var+t62*t72*vwe_var+t62*t68*vwn_var |
Definition at line 88 of file Q_airdata.c.
float aos_var = t77*t87*vd_var+t77*t80*ve_var+t77*t83*vn_var+t77*t87*vwd_var+t77*t80*vwe_var+t77*t83*vwn_var |
Definition at line 89 of file Q_airdata.c.
float t10 = q2*q3*2.0f |
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float t11 = vn-vwn |
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float t13 = q0*q2*2.0f |
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float t14 = q1*q3*2.0f |
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float t15 = q0*q3*2.0f |
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float t16 = q1*q2*2.0f |
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float t3 = ve-vwe |
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float t4 = q0*q0 |
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float t41 = 1.0f/t40 |
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float t5 = q1*q1 |
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float t57 = 1.0f/(t17*t17) |
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float t58 = 1.0f/t17 |
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float t6 = q2*q2 |
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float t61 = t60+1.0f |
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float t62 = 1.0f/(t61*t61) |
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float t7 = q3*q3 |
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float t76 = t75+1.0f |
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float t77 = 1.0f/(t76*t76) |
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float t8 = vd-vwd |
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float t9 = q0*q1*2.0f |
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float tas_var = t41*t47*vd_var*0.25f+t41*t51*ve_var*0.25f+t41*t55*vn_var*0.25f+t41*t47*vwd_var*0.25f+t41*t51*vwe_var*0.25f+t41*t55*vwn_var*0.25f |
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