5e92091e-4aa0-4d12-bddc-9dc3d36e6fa1 13 9 12 decimal

&[DATE] &[TIME] - &[FILENAME]

Solving NASA(h)

altitude[m] from measured kPa

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h NASA 101.29 288.14 0.00649 h * - 288.08 / (5.256^* 1000 - h ≤ (h 11000 ≤ (& 22.65 1.73 0.000157 h * - exp * 11000 h ≤ (h 25000 ≤ (& 2.488 141.89 0.00299 h * + 216.6 / (11.388 -^* cases :

L H N xd U 0 : dx H L - N 1 - / : 12 mat i 1 N range U i el L dx - (dx i * + eval : for U 31 line :

You may range <= from 25000

L 60000 NASA : H 101.325 : N 201 : 13 mat

u L H N xd :

sol i 1 u rows range m_altitude i el h NASA u i el - 0 ≡ h 0100000 solve : for u 1 round vectorize m_altitude 0 round vectorize augment 21 line :

t0 1 time :

NASA(h) solved [m_altitude] from measured kPa

sol 101.325 10000 101.325 10000 - 2 2 mat 2 1 sys

sol 11 mat evaluate/export sol ≡

1 time t0 - 45 s *