Proof LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES (Closes #224) (#316)

* Proof LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES (#224)

* 👌 Follow "triple space" rule for indentation

Comanche055/LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES.agc

@@ -43,13 +43,6 @@
 #	A NINTH DEGREE POLYNOMIAL APPROXIMATION WHICH IS VALID OVER A 15
 #	DAY INTERVAL BEGINNING SHORTLY BEFORE LAUNCH.  THEREFORE THE TIME
 #	INPUT BY THE USER SHOULD FALL WITHIN THIS 15 DAY INTERVAL.
-##	The 9th-degree polynomial spoken of here is a pad load, meaning
-##	that it is not actually hardcoded into the software.  Additional
-##	information about calculating the polynomial can be found on the
-##	<a href="http://nassp.sourceforge.net/wiki/Lunar_Ephemeris_Polynomials">
-##	<b>Orbiter</b> NASSP wiki</a>, as well as information about calculation
-##	of the <a href="http://nassp.sourceforge.net/wiki/Solar_Ephemeris">
-##	solar ephemerides</a>.
 #
 #	LSPOS COMPUTES THE POSITION VECTORS OF THE SUN AND THE MOON.
 #
@@ -69,44 +62,43 @@
 #
 #	1) SPECIFIED GROUND ELAPSED TIME IN CS x B-28 LOADED IN MPAC.
 #
-#	2) TIMEMO -- TIME AT THE CENTER OF THE RANGE OVER WHICH THE LUNAR
-#	POSITION POLYNOMIAL IS VALID IN CS x B-42.
+#	2) TIMEMO - TIME AT THE CENTER OF THE RANGE OVER WHICH THE LUNAR
+#	   POSITION POLYNOMIAL IS VALID IN CS x B-42.
 #
-#	3) VECOEM -- VECTOR COEFFICIENTS OF THE LUNAR POSITION POLYNOMIAL
-#	LOADED IN DESCENDING SEQUENCE IN METERS/CS**N x B-2
+#	3) VECOEM - VECTOR COEFFICIENTS OF THE LUNAR POSITION POLYNOMIAL
+#	   LOADED IN DESCENDING SEQUENCE IN METERS/CS**N x B-2
 #
-#	4) RESO -- POSITION VECTOR OF THE SUN RELATIVE TO THE EARTH AT
-#	TIMEMO IN METERS x B-38
+#	4) RESO - POSITION VECTOR OF THE SUN RELATIVE TO THE EARTH AT
+#	   TIMEMO IN METERS x B-38.
 #
-#	5) VESO -- VELOCITY VECTOR OF THE SUN RELATIVE TO THE EARTH AT
-#	TIMEMO IN METERS/CS x B-9
+#	5) VESO - VELOCITY VECTOR OF THE SUN RELATIVE TO THE EARTH AT
+#	   TIMEMO IN METERS/CS x B-9.
 #
-#	6) OMEGAES -- ANGULAR VELOCITY OF THE VECTOR RESO AT TIMEMO IN
-#	REV/CS x B+26
+#	6) OMEGAES - ANGULAR VELOCITY OF THE VECTOR RESO AT TIMEMO IN
+#	   REV/CS x B+26.
 #
 #	ALL EXCEPT THE FIRST INPUT ARE INCLUDED IN THE PRE-LAUNCH
 #	ERASABLE DATA LOAD.
 #
-# OUTPUT -- LSPOS
+# OUTPUT - LSPOS
 # Page 786
-#
 #	1) 2D OF VAC AREA CONTAINS THE POSITION VECTOR OF THE SUN RELATIVE
-#	TO THE EARTH AT TIME INPUT BY THE USER IN METERS x B-38.
+#	   TO THE EARTH AT TIME INPUT BY THE USER IN METERS x B-38.
 #
 #	2) MPAC CONTAINS THE POSITION VECTOR OF THE MOON RELATIVE TO THE
-#	EARTH AT TIME INPUT BY THE USER IN METERS x B-29
+#	   EARTH AT TIME INPUT BY THE USER IN METERS x B-29.
 #
-# OUTPUT -- LUNPOS
+# OUTPUT - LUNPOS
 #
 #	MPAC CONTAINS THE POSITION VECTOR OF THE MOON RELATIVE TO THE
-#	EARTH AT THE TIME INPUT BY USER IN METERS x B-29
+#	EARTH AT THE TIME INPUT BY USER IN METERS x B-29.
 #
-# OUTPUT -- LUNVEL
+# OUTPUT - LUNVEL
 #
 #	MPAC CONTAINS THE VELOCITY VECTOR OF THE MOON RELATIVE TO THE
-#	EARTH AT THE TIME INPUT BY THE USER IN METERS/CS x B-7
+#	EARTH AT THE TIME INPUT BY THE USER IN METERS/CS x B-7.
 #
-# OUTPUT -- SOLPOS
+# OUTPUT - SOLPOS
 #
 #	MPAC CONTAINS THE POSITION VECTOR OF THE SUN RELATIVE TO THE EARTH
 #	AT TIME INPUT BY THE USER IN METERS x B-38.
@@ -120,11 +112,9 @@
 #	THE VAC AREA IS USED FOR STORAGE OF INTERMEDIATE AND FINAL RESULTS
 #	OF COMPUTATIONS.
 #
-#	S1, X1, AND X2 ARE USED BY THESE SUBROUTINES.
-#
+#	S1, X1 AND X2 ARE USED BY THESE SUBROUTINES.
 #	PRELAUNCH ERASABLE DATA LOAD ARE ONLY ERASABLE STORAGE USED BY
 #	THESE SUBROUTINES.
-#
 #	RESTARTS DURING OPERATION OF THESE SUBROUTINES MUST BE HANDLED BY
 #	THE USER.
 
@@ -206,6 +196,3 @@ VEMA		VXSC
 NINEB4		2DEC	9.0 B-4
 
 ONEB4		2DEC	1.0 B-4
-
-
-