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Proof read #214: INFLIGHT_ALIGNMENT_ROUTINES (#369)

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* 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
This commit is contained in:
Tim Joosten 2019-01-22 01:23:10 +01:00 committed by James Harris
parent d203c2795d
commit ecc339601d
1 changed files with 7 additions and 7 deletions
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14
Comanche055/INFLIGHT_ALIGNMENT_ROUTINES.agc
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@ -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