From 36e094c97715c58f624be3e8bccc67778eadadc3 Mon Sep 17 00:00:00 2001 From: scottma Date: Fri, 8 May 2026 14:56:56 +0000 Subject: [PATCH 1/2] Edit _3gpp-nr-nrm-ntnfunction.yang --- yang-models/_3gpp-nr-nrm-ntnfunction.yang | 20 ++++++++------------ 1 file changed, 8 insertions(+), 12 deletions(-) diff --git a/yang-models/_3gpp-nr-nrm-ntnfunction.yang b/yang-models/_3gpp-nr-nrm-ntnfunction.yang index 5abe98f6..c91ac512 100644 --- a/yang-models/_3gpp-nr-nrm-ntnfunction.yang +++ b/yang-models/_3gpp-nr-nrm-ntnfunction.yang @@ -18,6 +18,7 @@ module _3gpp-nr-nrm-ntnfunction { TTA, TTC). All rights reserved."; reference "3GPP TS 28.541"; + revision 2024-05-06 { reference CR-1716 ; } revision 2024-05-24 { reference CR-1273 ; } feature NTNFunctionUnderSubNetwork { @@ -116,8 +117,7 @@ module _3gpp-nr-nrm-ntnfunction { config false; default 0; units meter; - description "Satellite orbital parameter: semi major axis alpha, - see NIMA TR 8350.2. + description "Satellite orbital parameter: semi major axis alpha. Step of 4.249 * 10**-3 m. Actual value = 6500000 + field value * (4.249 * 10**-3)."; } @@ -128,8 +128,7 @@ module _3gpp-nr-nrm-ntnfunction { } config false; default 0; - description "Satellite orbital parameter: eccentricity e, - see NIMA TR 8350.2. + description "Satellite orbital parameter: eccentricity e. Step 1.431 * 10**-8. Actual value = field value * (1.431 * 10**-8)."; } @@ -141,8 +140,7 @@ module _3gpp-nr-nrm-ntnfunction { config false; default 0; units radian; - description "Satellite orbital parameter: argument of periapsis omega, - see NIMA TR 8350.2. + description "Satellite orbital parameter: argument of periapsis omega. Step of 2.341* 10**-8 rad. Actual value = field value * (2.341* 10**-8)."; } @@ -155,7 +153,7 @@ module _3gpp-nr-nrm-ntnfunction { default 0; units radian; description "Satellite orbital parameter: longitude of ascending node - OMEGA, see NIMA TR 8350.2. + omega. Step of 2.341* 10**-8 rad. Actual value = field value * (2.341* 10**-8)."; } @@ -167,8 +165,7 @@ module _3gpp-nr-nrm-ntnfunction { config false; default 0; units radian; - description "Satellite orbital parameter: inclination i, - see NIMA TR 8350.2. + description "Satellite orbital parameter: inclination i. Step of 2.341* 10**-8 rad. Actual value = field value * (2.341* 10**-8)."; } @@ -180,8 +177,7 @@ module _3gpp-nr-nrm-ntnfunction { config false; default 0; units radian; - description "Satellite orbital parameter: Mean anomaly M at epoch time, - see NIMA TR 8350.2. + description "Satellite orbital parameter: Mean anomaly M at epoch time. Step of 2.341* 10**-8 rad. Actual value = field value * (2.341* 10**-8)."; } @@ -221,7 +217,7 @@ module _3gpp-nr-nrm-ntnfunction { list orbital { description "It indicates ephemeris is in orbital parameter ephemeris - format, as specified in NIMA TR 8350.2"; + format."; max-elements 1; config false; uses OrbitalGrp; -- GitLab From 3aad78abadd4236a44e7b4ec7204dfde67f8c1b0 Mon Sep 17 00:00:00 2001 From: scottma Date: Fri, 8 May 2026 15:00:06 +0000 Subject: [PATCH 2/2] Edit _3gpp-nr-nrm-ntnfunction.yang --- yang-models/_3gpp-nr-nrm-ntnfunction.yang | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/yang-models/_3gpp-nr-nrm-ntnfunction.yang b/yang-models/_3gpp-nr-nrm-ntnfunction.yang index c91ac512..61bf63a2 100644 --- a/yang-models/_3gpp-nr-nrm-ntnfunction.yang +++ b/yang-models/_3gpp-nr-nrm-ntnfunction.yang @@ -18,7 +18,7 @@ module _3gpp-nr-nrm-ntnfunction { TTA, TTC). All rights reserved."; reference "3GPP TS 28.541"; - revision 2024-05-06 { reference CR-1716 ; } + revision 2026-05-06 { reference CR-1716 ; } revision 2024-05-24 { reference CR-1273 ; } feature NTNFunctionUnderSubNetwork { -- GitLab