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CL_op_frozenOrbit

Eccentricity and argument of periapsis of a frozen orbit

Calling Sequence

[ecc, pom] = CL_op_frozenOrbit(sma, inc [[, er, j1jn]])

Description

Parameters

sma:

Semi major axis [m] (1xN or 1x1)

inc:

Inclination [rad] (1xN or 1x1)

er:

(optional) Equatorial radius. Default: %CL_eqRad. [m] (1x1).

j1jn:

(optional) Vector of zonal coefficients J1 to Jn (1xNz or Nzx1). Default is %CL_j1jn(1:3).

ecc:

Mean eccentricity (1xN)

pom:

Mean argument of periapsis [rad] (1xN)

Authors

Examples

sma = [7000.e3, 7300.e3];
inc = CL_deg2rad(98);
[ecc,pom] = CL_op_frozenOrbit(sma,inc)
j1jn = CL_dataGet("j1jn");
j1j20 = j1jn(1:20);
[ecc,pom] = CL_op_frozenOrbit(sma,inc,j1jn=j1j20)

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