Complete the table below (all grey cells can be completed in excel): + t It Rt 2= Ap/ At L(orbit) = mr20 SL [flash] [gridinch] [degree] r = 1/2(r, + riti) [gridinch] [deg/flash] [puck gridinch?/flash] 0 3 +- 0.2 110 +- 0.3 3.15 20 180 3.3 +- 0.3 130 +- 0.4 3.55 16 174.24 2 3.8 +- 0.3 146 +- 0.3 4.1 10 144.4 3 4.4 +- 0.2 156 +- 0.4 4.55 8 154.88 4 4.7 +- 0.3 164 +- 0.3 4.7 9 198.81 5 4.7 +- 0.4 173 +- 0.3 4.6 8 176.72 6 4.5 +- 0.3 181 +- 0.2 4.25 11 222.75 7 4.0 +- 0.3 192 +- 0.3 3.75 13 208 8 3.5 +- 0.2 205 +- 0.3 3.35 16 196 9 3.2 +- 0.3 221 +- 0.4 3.2 19 204.48 10 3.2 +- 0.3 241 +- 0.3 3.3 18 184.32 11 3.4 +- 0.3 259 +- 0.3 Show the error propagation equations for of and or