* 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
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@ -36,15 +36,15 @@
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# CALCGTA COMPUTES THE GYRO TORQUE ANGLES REQUIRED TO BRING THE STABLE MEMBER INTO THE DESIRED ORIENTATION.
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# CALCGTA COMPUTES THE GYRO TORQUE ANGLES REQUIRED TO BRING THE STABLE MEMBER INTO THE DESIRED ORIENTATION.
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#
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#
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# THE INPUT IS THE DESIRED STABLE MEMBER COORDINATES REFERRED TO PRESENT STABLE MEMBER COORDINATES. THE THREE
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# THE INPUT IS THE DESIRED STABLE MEMBER COORDINATES REFERRED TO PRESENT STABLE MEMBER COORDINATES. THE THREE
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# HALF-UNIT VECTORS ARE STORED AT XDC, YDC, AND ZDC.
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# HALF-UNIT VECTORS ARE STORED AT XDC, YDC, AND ZDC.
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#
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#
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# THE OUTPUTS ARE THE THREE GYRO TORQUE ANGLES TO BE APPLIED TO THE Y, Z, AND X GYROS AND ARE STORED DP AT IGC,
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# THE OUTPUTS ARE THE THREE GYRO TORQUING ANGLES TO BE APPLIED TO THE Y, Z, AND X GYROS AND ARE STORED DP AT IGC,
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# MGC, AND OGC RESPECTIVELY.
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# MGC, AND OGC RESPECTIVELY.
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COUNT 23/INFLT
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COUNT 23/INFLT
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CALCGTA ITA DLOAD # PUSHDOWN 00-03, 16D-27D, 34D-37D
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CALCGTA ITA DLOAD # PUSHDOWN 00-03,16D-27D,34D-37D
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S2 # XDC = (XD1 XD2 XD3)
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S2 # XDC = (XD1 XD2 XD3)
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XDC # YDC = (YD1 YD2 YD3)
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XDC # YDC = (YD1 YD2 YD3)
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PDDL PDDL # ZDC = (ZD1 ZD2 ZD3)
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PDDL PDDL # ZDC = (ZD1 ZD2 ZD3)
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@ -97,7 +97,7 @@ CALCGTA ITA DLOAD # PUSHDOWN 00-03, 16D-27D, 34D-37D
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#
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#
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# THE INPUTS ARE SIN/4 AND COS/4 STORED DP AT SINTH AND COSTH.
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# THE INPUTS ARE SIN/4 AND COS/4 STORED DP AT SINTH AND COSTH.
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#
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#
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# THE OUTPUT IS THE CALCULATED ANGLE BETWEEN +.5 AND -.5 REVOLUTIONS AND STORED AT THETA. THE OUTPUT IS ALSO
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# THE OUTPUT IS THE CALCULATED ANGLE BETWEEN +.5 AND -.5 REVOLUTIONS AND STORED AT THETA. THE OUTPUT IS ALSO
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# AVAILABLE AT MPAC.
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# AVAILABLE AT MPAC.
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ARCTRIG DLOAD ABS # PUSHDOWN 16D-21D
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ARCTRIG DLOAD ABS # PUSHDOWN 16D-21D
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@ -140,13 +140,13 @@ TRIG2 DLOAD SIGN # (135,-135)
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# Page 1359
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# Page 1359
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# CALCGA COMPUTES THE CDU DRIVING ANGLES REQUIRED TO BRING THE STABLE MEMBER INTO THE DESIRED ORIENTATION.
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# CALCGA COMPUTES THE CDU DRIVING ANGLES REQUIRED TO BRING THE STABLE MEMBER INTO THE DESIRED ORIENTATION.
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#
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#
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# THE INPUTS ARE 1) THE NAVIGATION BASE COORDINATES REFERRED TO ANY COORDINATE SYSTEM. THE THREE HALF-UNIT
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# THE INPUTS ARE 1) THE NAVIGATION BASE COORDINATES REFERRED TO ANY COORDINATE SYSTEM. THE THREE HALF-UNIT
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# VECTORS ARE STORED AT XNB, YNB, AND ZNB. 2) THE DESIRED STABLE MEMBER COORDINATES REFERRED TO THE SAME
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# VECTORS ARE STORED AT XNB, YNB, AND ZNB. 2) THE DESIRED STABLE MEMBER COORDINATES REFERRED TO THE SAME
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# COORDINATE SYSTEM ARE STORED AT XSM, YSM, AND ZSM.
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# COORDINATE SYSTEM ARE STORED AT XSM, YSM, AND ZSM.
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#
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#
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# THE OUTPUTS ARE THE THREE CDU DRIVING ANGLES AND ARE STORED SP AT THETAD, THETAD +1, AND THETAD +2.
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# THE OUTPUTS ARE THE THREE CDU DRIVING ANGLES AND ARE STORED SP AT THETAD, THETAD +1, AND THETAD +2.
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CALCGA SETPD # PUSHDOWN 00-05, 16D-21D, 34D-37D
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CALCGA SETPD # PUSHDOWN 00-05, 16D-21D, 34D-37D
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0
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0
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VLOAD VXV
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VLOAD VXV
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XNB # XNB = OGA (OUTER GIMBAL AXIS)
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XNB # XNB = OGA (OUTER GIMBAL AXIS)
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@ -222,7 +222,7 @@ GIMLOCK1 EXIT
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# THE OUTPUT DEFINES COORDINATE SYSTEM A REFERRED TO COORDINATE SYSTEM B. THE THREE HALF-UNIT VECTORS ARE STORED
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# THE OUTPUT DEFINES COORDINATE SYSTEM A REFERRED TO COORDINATE SYSTEM B. THE THREE HALF-UNIT VECTORS ARE STORED
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# AT LOCATIONS XDC, XDC +6, XDC +12D, AND STARAD, STARAD +6, STARAD +12D.
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# AT LOCATIONS XDC, XDC +6, XDC +12D, AND STARAD, STARAD +6, STARAD +12D.
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AXISGEN AXT,1 SSP # PUSHDOWN 00-30D, 34D-37D
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AXISGEN AXT,1 SSP # PUSHDOWN 00-30D, 34D-37D
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STARAD +6
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STARAD +6
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S1
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S1
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STARAD -6
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STARAD -6
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