From f41b108e44b2b26ecc72977e82e695e5d9c94d9b Mon Sep 17 00:00:00 2001
From: Connor Powers <20464743+connor-powers@users.noreply.github.com>
Date: Sun, 18 May 2025 22:33:46 -0700
Subject: [PATCH] Update README.md

updating argument of perigee to argument of periapsis
---
 README.md | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/README.md b/README.md
index b0382c6..81a2814 100644
--- a/README.md
+++ b/README.md
@@ -33,7 +33,7 @@
 
    - Continuous (low) thrust orbit raising/lowering between circular orbits
    
-   - Continuous (low) thrust maneuvers to change argument of perigee
+   - Continuous (low) thrust maneuvers to change argument of periapsis
       
       - Note: Thrust profiles of argument of periapsis change maneuvers are calculated assuming a "continuous" maneuver takes place (i.e., a burn arc angle $\alpha = \pi/2$ radians in https://apps.dtic.mil/sti/tr/pdf/ADA384536.pdf). Therefore it is not recommended to use this feature outside of parameter ranges where this assumption does not hold. Maneuvers that take place over a fraction of an orbit are not recommended.