/** Options for Dspace */
export interface DspaceOptions {
    irez: number;
    d2201: number;
    d2211: number;
    d3210: number;
    d3222: number;
    d4410: number;
    d4422: number;
    d5220: number;
    d5232: number;
    d5421: number;
    d5433: number;
    dedt: number;
    del1: number;
    del2: number;
    del3: number;
    didt: number;
    dmdt: number;
    dnodt: number;
    domdt: number;
    argpo: number;
    argpdot: number;
    tc: number;
    gsto: number;
    xfact: number;
    xlamo: number;
    no: number;
    atime: number;
    em: number;
    argpm: number;
    inclm: number;
    xli: number;
    mm: number;
    xni: number;
    nodem: number;
    nm: number;
}
/** Output from Dspace computation */
export interface DspaceOutput {
    atime: number;
    em: number;
    argpm: number;
    inclm: number;
    xli: number;
    mm: number;
    xni: number;
    nodem: number;
    dndt: number;
    nm: number;
}
/**
 *                           procedure dspace
 *
 *  this procedure provides deep space contributions to mean elements for
 *    perturbing third body.  these effects have been averaged over one
 *    revolution of the sun and moon.  for earth resonance effects, the
 *    effects have been averaged over no revolutions of the satellite.
 *    (mean motion)
 *
 *  author        : david vallado                  719-573-2600   28 jun 2005
 *
 *  inputs        :
 *    d2201, d2211, d3210, d3222, d4410, d4422, d5220, d5232, d5421, d5433 -
 *    dedt        -
 *    del1, del2, del3  -
 *    didt        -
 *    dmdt        -
 *    dnodt       -
 *    domdt       -
 *    irez        - flag for resonance           0-none, 1-one day, 2-half day
 *    argpo       - argument of perigee
 *    argpdot     - argument of perigee dot (rate)
 *    t           - time
 *    tc          -
 *    gsto        - gst
 *    xfact       -
 *    xlamo       -
 *    no          - mean motion
 *    atime       -
 *    em          - eccentricity
 *    ft          -
 *    argpm       - argument of perigee
 *    inclm       - inclination
 *    xli         -
 *    mm          - mean anomaly
 *    xni         - mean motion
 *    nodem       - right ascension of ascending node
 *
 *  outputs       :
 *    atime       -
 *    em          - eccentricity
 *    argpm       - argument of perigee
 *    inclm       - inclination
 *    xli         -
 *    mm          - mean anomaly
 *    xni         -
 *    nodem       - right ascension of ascending node
 *    dndt        -
 *    nm          - mean motion
 *
 *  locals        :
 *    delt        -
 *    ft          -
 *    theta       -
 *    x2li        -
 *    x2omi       -
 *    xl          -
 *    xldot       -
 *    xnddt       -
 *    xndt        -
 *    xomi        -
 *
 *  coupling      :
 *    none        -
 *
 *  references    :
 *    hoots, roehrich, norad spacetrack report #3 1980
 *    hoots, norad spacetrack report #6 1986
 *    hoots, schumacher and glover 2004
 *    vallado, crawford, hujsak, kelso  2006
 * @param options - options explaining how to compute
 * @param tsince - time since epoch
 * @returns - computed values
 */
export declare function dspace(options: DspaceOptions, tsince: number): DspaceOutput;
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