Merge branch 'master' into rename

Comanche055/CONIC_SUBROUTINES.agc

@@ -69,7 +69,7 @@
 # FUNCTIONAL DESCRIPTION --
 #	THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND THE DESIRED TRANSFER TIME THROUGH WHICH THE STATE IS TO
 #	BE UPDATED ALONG A CONIC TRAJECTORY, COMPUTES THE NEW, UPDATED STATE VECTOR.  THE TRAJECTORY MAY BE ANY CONIC
-#	SECTION -- CIRCULAR, ELLIPTIC, PARABOLIC, HYPERPOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON. THE
+#	SECTION -- CIRCULAR, ELLIPTIC, PARABOLIC, HYPERBOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON. THE
 #	USE OF THE SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT
 #	INTRODUCING ANY CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.  AN ITERATION
 #	TECHNIQUE IS UTILIZED IN THE COMPUTATION.
@@ -106,7 +106,7 @@
 #							RESPECTIVELY, IS THE CENTRAL BODY
 #	TAU		+28			DESIRED TRANSFER TIME IN CENTISECONDS (DP)
 #							MAY BE POS OR NEG AND ABSOLUTE VALUE MAY BE GREATER OR LESS THAN ONE ORBITAL PERIOD.
-#	XKEPNEW		+17 FOR EARTH		DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WTIH THAT OF TAU.
+#	XKEPNEW		+17 FOR EARTH		DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WITH THAT OF TAU.
 #			+16 FOR MOON			AND ABS VALUE SHOULD BE LESS THAN THAT CORRESPONDING TO A PERIOD, VIZ, 2PI SQRT(SEMI-
 #							MAJOR AXIS), FOR SPEED OF CONVERGENCE, BUT IF EITHER CONDITION FAILS, XKEPNEW IS RESET
 #							BY KEPLER TO A POOR BUT VALID GUESS.
@@ -284,9 +284,9 @@
 # FUNCTIONAL DESCRIPTION --
 #	THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED TRUE-ANOMALY-DIFFERENCE THROUGH WHICH THE
 #	STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
-#	PROVIDES THE OPTION OF COMUTING THE NEW UPDATED STATE VECTOR.  THE RESULTING TRAJECTORY MAY BE A SECTION OF A
+#	PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR.  THE RESULTING TRAJECTORY MAY BE A SECTION OF A
 #	CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON.  THE USE OF THE SUBROUTINE CAN BE
-# 	EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WTIHOUT INTRODUCING ANY CODING CHANGES,
+# 	EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
 #	ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
 #
 # THE RESTRICTIONS ARE --
@@ -387,7 +387,7 @@
 #	STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
 #	PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR.  THE RESULTING TRAJECTORY MAY BE A SECTION OF A
 #	CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON.  THE USE OF THE SUBROUTINE CAN BE
-#	EXTENDED USING OTHER PRIMARY BODIES BY SIMMPE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
+#	EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
 #	ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
 #
 #	IF THE DESIRED RADIUS IS BEYOND THE RADIUS OF APOCENTER OF THE CONIC OR BELOW THE RADIUS OF PERICENTER,
@@ -1776,7 +1776,7 @@ MUTABLE		2DEC*	3.986032 E10 B-36*	# MUE
 
 LDPOSMAX	EQUALS 	LODPMAX			# DPPOSMAX IN LOW MEMORY.
 
-# ERASABLE ASSIGNEMENTS
+# ERASABLE ASSIGNMENTS
 
 # KEPLER SUBROUTINE
 
@@ -1825,7 +1825,7 @@ KEPC2		EQUALS	36D
 # R2VEC		ERASE 	+5
 # TDESIRED	ERASE	+1
 # GEOMSGN	ERASE	+0
-# GUESSW			# 0 IF COGA GUESS AVIABLE, 1 IF NOT
+# GUESSW			# 0 IF COGA GUESS AVAILABLE, 1 IF NOT
 # COGA		ERASE	+1	# INPUT ONLY IF GUESS IS ZERO.
 # NORMSW			# 0 IF UN TO BE COMPUTED, 1 IF UN INPUT
 # UN		ERASE	+5	# ONLY USED IF NORMSW IS 1