From ecc339601df4a8a136f2477082df4c21df4761d9 Mon Sep 17 00:00:00 2001 From: Tim Joosten Date: Tue, 22 Jan 2019 01:23:10 +0100 Subject: [PATCH] Proof read #214: INFLIGHT_ALIGNMENT_ROUTINES (#369) * Proof: INFLIGHT_ALIGNMENT_ROUTINES.agc - P1355 Removed an unnecessarily space SEE: https://git.io/fhgW4 SEE: https://bit.ly/2HrJTu0 R0007 [SIGNED OFF]: Tim Joosten * Proof: INFLIGHT_ALIGNMENT_ROUTINES.agc - P1355 Replaced the word TORQUE with TORQUING and replaced dots woth comma's SEE: https://git.io/fhglL SEE: https://bit.ly/2HrJTu0 R0010 [SIGNED OFF]: Tim Joosten * Proof: INFLIGHT_ALIGNMENT_ROUTINES.agc - P1335 Applied several fixes on R0015. SEE: https://bit.ly/2HrJTu0 R0015 [SIGNED OFF]: Tim Joosten * Proof: INFLIGHT_ALIGNMENt_ROUTINES.agc - P1357 Remove unnecessarily space. SEE: https://git.io/fhglb SEE: https://bit.ly/2AU79v6 R0057 [SIGNED OFF]: Tim Joosten * Proof: INFLIGHT_ALIGNMENT_ROUTINES.agc - P1359 Removed unnecessarily space SEE: https://bit.ly/2RZ7WV9 R0092 SEE: https://git.io/fhg8z [SIGNED OFF]: Tim Joosten * Proof: INFLIGT_ALIGNMENT_ROUTINES.agc - P1359 Add missing space. SEE: https://git.io/fhg8P SEE: https://bit.ly/2RZ7WV9 R0099 [SIGNED OFF]: Tim Joosten * Proof: INFLIGHT_ALIGNMENT_ROUTINES.agc - P1361 Add missing space SEE: https://git.io/fhg4t SEE: https://bit.ly/2FNoOb6 R0165 [SIGNED OFF]: Tim Joosten * revert , -> . on line 42 --- Comanche055/INFLIGHT_ALIGNMENT_ROUTINES.agc | 14 +++++++------- 1 file changed, 7 insertions(+), 7 deletions(-) diff --git a/Comanche055/INFLIGHT_ALIGNMENT_ROUTINES.agc b/Comanche055/INFLIGHT_ALIGNMENT_ROUTINES.agc index fcd90ac..eab2d02 100644 --- a/Comanche055/INFLIGHT_ALIGNMENT_ROUTINES.agc +++ b/Comanche055/INFLIGHT_ALIGNMENT_ROUTINES.agc @@ -36,15 +36,15 @@ # CALCGTA COMPUTES THE GYRO TORQUE ANGLES REQUIRED TO BRING THE STABLE MEMBER INTO THE DESIRED ORIENTATION. # -# THE INPUT IS THE DESIRED STABLE MEMBER COORDINATES REFERRED TO PRESENT STABLE MEMBER COORDINATES. THE THREE +# THE INPUT IS THE DESIRED STABLE MEMBER COORDINATES REFERRED TO PRESENT STABLE MEMBER COORDINATES. THE THREE # HALF-UNIT VECTORS ARE STORED AT XDC, YDC, AND ZDC. # -# THE OUTPUTS ARE THE THREE GYRO TORQUE ANGLES TO BE APPLIED TO THE Y, Z, AND X GYROS AND ARE STORED DP AT IGC, +# THE OUTPUTS ARE THE THREE GYRO TORQUING ANGLES TO BE APPLIED TO THE Y, Z, AND X GYROS AND ARE STORED DP AT IGC, # MGC, AND OGC RESPECTIVELY. COUNT 23/INFLT -CALCGTA ITA DLOAD # PUSHDOWN 00-03, 16D-27D, 34D-37D +CALCGTA ITA DLOAD # PUSHDOWN 00-03,16D-27D,34D-37D S2 # XDC = (XD1 XD2 XD3) XDC # YDC = (YD1 YD2 YD3) PDDL PDDL # ZDC = (ZD1 ZD2 ZD3) @@ -97,7 +97,7 @@ CALCGTA ITA DLOAD # PUSHDOWN 00-03, 16D-27D, 34D-37D # # THE INPUTS ARE SIN/4 AND COS/4 STORED DP AT SINTH AND COSTH. # -# THE OUTPUT IS THE CALCULATED ANGLE BETWEEN +.5 AND -.5 REVOLUTIONS AND STORED AT THETA. THE OUTPUT IS ALSO +# THE OUTPUT IS THE CALCULATED ANGLE BETWEEN +.5 AND -.5 REVOLUTIONS AND STORED AT THETA. THE OUTPUT IS ALSO # AVAILABLE AT MPAC. ARCTRIG DLOAD ABS # PUSHDOWN 16D-21D @@ -140,13 +140,13 @@ TRIG2 DLOAD SIGN # (135,-135) # Page 1359 # CALCGA COMPUTES THE CDU DRIVING ANGLES REQUIRED TO BRING THE STABLE MEMBER INTO THE DESIRED ORIENTATION. # -# THE INPUTS ARE 1) THE NAVIGATION BASE COORDINATES REFERRED TO ANY COORDINATE SYSTEM. THE THREE HALF-UNIT +# THE INPUTS ARE 1) THE NAVIGATION BASE COORDINATES REFERRED TO ANY COORDINATE SYSTEM. THE THREE HALF-UNIT # VECTORS ARE STORED AT XNB, YNB, AND ZNB. 2) THE DESIRED STABLE MEMBER COORDINATES REFERRED TO THE SAME # COORDINATE SYSTEM ARE STORED AT XSM, YSM, AND ZSM. # # THE OUTPUTS ARE THE THREE CDU DRIVING ANGLES AND ARE STORED SP AT THETAD, THETAD +1, AND THETAD +2. -CALCGA SETPD # PUSHDOWN 00-05, 16D-21D, 34D-37D +CALCGA SETPD # PUSHDOWN 00-05, 16D-21D, 34D-37D 0 VLOAD VXV XNB # XNB = OGA (OUTER GIMBAL AXIS) @@ -222,7 +222,7 @@ GIMLOCK1 EXIT # THE OUTPUT DEFINES COORDINATE SYSTEM A REFERRED TO COORDINATE SYSTEM B. THE THREE HALF-UNIT VECTORS ARE STORED # AT LOCATIONS XDC, XDC +6, XDC +12D, AND STARAD, STARAD +6, STARAD +12D. -AXISGEN AXT,1 SSP # PUSHDOWN 00-30D, 34D-37D +AXISGEN AXT,1 SSP # PUSHDOWN 00-30D, 34D-37D STARAD +6 S1 STARAD -6