Commit 1cdb6090 authored by lengyelb's avatar lengyelb
Browse files

Made ephemeris readwrite, common in r19,20

parent 8e1244f9

yang-models/_3gpp-nr-nrm-ntnfunction.yang

+6 −17
Original line number Diff line number Diff line
@@ -15,10 +15,11 @@ module _3gpp-nr-nrm-ntnfunction { 
  contact "https://www.3gpp.org/DynaReport/TSG-WG--S5--officials.htm?Itemid=464";

  description "Implements support the C-SON function of Capacity and 

    Coverage optimization .

    Copyright 2025, 3GPP Organizational Partners (ARIB, ATIS, CCSA, ETSI, TSDSI, 

    Copyright 2026, 3GPP Organizational Partners (ARIB, ATIS, CCSA, ETSI, TSDSI, 

    TTA, TTC). All rights reserved.";

  reference "3GPP TS 28.541";

  

  revision 2026-02-02 { reference "CR-1682 CR-1683"; } //Common in r19, r20

  revision 2025-03-27 { reference CR-1512; }

  revision 2025-02-17 { reference CR-1479 ; }

  revision 2024-05-24 { reference CR-1273 ; }
@@ -40,7 +41,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type uint32 {

        range 0..604800;

      }

      config false;

      default 0;

      units meter;

      description "X, Y, Z coordinate of satellite position state vector
@@ -52,7 +52,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type uint32 {

        range 0..604800;

      }

      config false;

      default 0;

      units meter;

      description "X, Y, Z coordinate of satellite position state vector
@@ -64,7 +63,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type uint32 {

        range 0..604800;

      }

      config false;

      default 0;

      units meter;

      description "X, Y, Z coordinate of satellite position state vector
@@ -76,7 +74,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type int32 {

        range -131072..131071;

      }

      config false;

      default 0;

      units meter/second;

      description "X, Y, Z coordinate of satellite velocity state vector
@@ -88,7 +85,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type int32 {

        range -131072..131071;

      }

      config false;

      default 0;

      units meter/second;

      description "X, Y, Z coordinate of satellite velocity state vector
@@ -100,7 +96,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type int32 {

        range -131072..131071;

      }

      config false;

      default 0;

      units meter/second;

      description "X, Y, Z coordinate of satellite velocity state vector
@@ -117,7 +112,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type uint64 {

        range 0..8589934591;

      }

      config false;

      default 0;

      units meter;

      description "Satellite orbital parameter: semi major axis alpha,
@@ -130,7 +124,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type int32 {

        range -524288..524287;

      }

      config false;

      default 0;

      description "Satellite orbital parameter: eccentricity e, 

        see NIMA TR 8350.2.
@@ -142,7 +135,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type uint32 {

        range 0..16777215;

      }

      config false;

      default 0;

      units radian;

      description "Satellite orbital parameter: argument of periapsis omega,
@@ -155,7 +147,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type uint32 {

        range 0..2097151;

      }

      config false;

      default 0;                

      units radian;

      description "Satellite orbital parameter: longitude of ascending node
@@ -168,7 +159,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type int32 {

        range -524288..524287;

      }

      config false;

      default 0;

      units radian;

      description "Satellite orbital parameter: inclination i,
@@ -181,7 +171,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type uint32 {

        range 0..16777215;

      }

      config false;

      default 0;

      units radian;

      description "Satellite orbital parameter: Mean anomaly M at epoch time,
@@ -201,7 +190,6 @@ module _3gpp-nr-nrm-ntnfunction { 
      type string {

        pattern "00([01][0-9][0-9])|(2[0-4][0-9]|(25[0-5]))";

      }

      config false;

      description "This attribute indicates satellite Id.number. 

        It shall be formatted as a fixed 5-digit string, padding with 

        leading digits '0' to complete a 5-digit length.
@@ -210,7 +198,6 @@ module _3gpp-nr-nrm-ntnfunction { 
    

    leaf epochTime {

      type yang:date-and-time;

      config false;

      description "It defines the ephemeris reference time.";

    }
@@ -219,7 +206,8 @@ module _3gpp-nr-nrm-ntnfunction { 
        description "It indicates ephemeris is in format of NTN payload 

          position and velocity state vectors.";

        max-elements 1;

        config false;

        key idx;

        leaf idx { type uint32; }

        uses PositionVelocityGrp;

      }
@@ -227,7 +215,8 @@ module _3gpp-nr-nrm-ntnfunction { 
        description "It indicates ephemeris is in orbital parameter ephemeris 

          format, as specified in NIMA TR 8350.2";

        max-elements 1;

        config false;

        key idx;

        leaf idx { type uint32; }

        uses OrbitalGrp;

      }

    }