Merge branch 'master' into rename

Luminary099/P32-P35_P72-P75.agc

@@ -30,11 +30,11 @@
 # COELLIPTIC SEQUENCE INITIATION (CSI) PROGRAMS (P32 AND P72)
 #
 # MOD NO -1		LOG SECTION -- P32-P35, P72-P75
-# MOD BY WHITE, P.	DATE 1 JUNE 67
+# MOD BY WHITE.P	DATE 1JUNE67
 #
 # PURPOSE
 
-#	(1)	TO CALCULATE PARAMETERS ASSOCIATED WTIH THE TIME FOLLOWING
+#	(1)	TO CALCULATE PARAMETERS ASSOCIATED WITH THE TIME FOLLOWING
 #		CONCENTRIC FLIGHT PLAN MANEUVERS -- THE CO-ELLIPTIC SEQUENCE
 #		INITIATION (CSI) MANEUVER AND THE CONSTANT DELTA ALTITUDE
 #		(CDH) MANEUVER.
@@ -44,14 +44,14 @@
 
 #	(3)	TO DISPLAY TO THE ASTRONAUT AND THE GROUND DEPENDENT VARIABLES
 #		ASSOCIATED WITH THE CONCENTRIC FLIGHT PLAN MANEUVERS FOR
-#		APPROVAL BY THE ASTRRONAUT/GROUND.
+#		APPROVAL BY THE ASTRONAUT/GROUND.
 
 #	(4)	TO STORE THE CSI TARGET PARAMETERS FOR USE BY THE DESIRED
 #		THRUSTING PROGRAM.
 #
 # ASSUMPTIONS
 
-#	(1)	AT A SELECTED TPI TIME THE LINE OF SIGNT BETWEEN THE ACTIVE
+#	(1)	AT A SELECTED TPI TIME THE LINE OF SIGHT BETWEEN THE ACTIVE
 #		AND PASSIVE VEHICLES IS SELECTED TO BE A PRESCRIBED ANGLE (E)
 #		FROM THE HORIZONTAL PLANE DEFINED BY THE ACTIVE VEHICLE
 #		POSITION.
@@ -72,7 +72,7 @@
 #		IGNITION.
 
 #	(6)	THE PERICENTER ALTITUDE OF THE ORBIT FOLLOWING CSI AND CDH
-#		MUST BE GREATER THAN 35,000 FT (LUNAR ORBIT) OR 85 NM (EARCH
+#		MUST BE GREATER THAN 35,000 FT (LUNAR ORBIT) OR 85 NM (EARTH
 #		ORBIT) FOR SUCCESSFUL COMPLETION OF THIS PROGRAM.
 
 #	(7)	THE CSI AND CDH MANEUVERS ARE ORIGINALLY ASSUMED TO BE
@@ -107,7 +107,7 @@
 #			CALCULATES THE MANEUVER PARAMETERS.  SET AT THE START OF
 #			EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
 #
-#			FINAL FLAG -- SELECTES FINAL PROGRAM DISPLAYS AFTER CREW HAS
+#			FINAL FLAG -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS
 #			COMPLETED THE FINAL MANEUVER COMPUTATION AND DISPLAY
 #			CYCLE.
 #