Exemplo n.º 1
0
def lambert_leg(P1, P2, i, j, t1, t2, tof, vrel=None, dv_launch=0.):
    """Compute a lambert leg from planet to planet.
    Arguments:
    p1 -- starting planet (str or PyKEP.planet object)
    p2 -- final planet (str or PyKEP.planet object)
    t0 -- start time of leg in MJD2000
    tof -- time of flight in days
    
    Keyword arguments:
    vrel -- caresian coordinates of the relative velocity before the flyby at p1
    dv_launch -- dv discounted at lunch (i.e. if vrel is None)
    rendezvous -- add final dv
    Returns:
    dV, vrel_out, where vrel_out is the relative velocity at the end of the leg at p2
    """

    ast1 = ASTEROIDS[P1]
    ast2 = ASTEROIDS[P2]

    r1 = state_asteroids.EPH[i][t1][0]
    v1 = state_asteroids.EPH[i][t1][1]
    r2 = state_asteroids.EPH[j][t2][0]
    v2 = state_asteroids.EPH[j][t2][1]

    lambert = kep.lambert_problem(r1, r2, tof * kep.DAY2SEC, ast1.mu_central_body, False, 0)

    vrel_in = tuple(map(lambda x, y: x - y, lambert.get_v1()[0], v1))
    vrel_out = tuple(map(lambda x, y: x - y, lambert.get_v2()[0], v2))

    dv_lambert = np.linalg.norm(vrel_out) + np.linalg.norm(vrel_in)

    a, _, _, dv_damon = kep.damon(vrel_in, vrel_out, tof*kep.DAY2SEC)
    m_star = kep.max_start_mass(np.linalg.norm(a), dv_damon, T_max, Isp)
    
    return dv_lambert, dv_damon, m_star
Exemplo n.º 2
0
def lambert_leg(P1, P2, t0, tof):
    
    ast1 = ASTEROIDS[P1]
    ast2 = ASTEROIDS[P2]

    r1, v1 = ast1.eph(kep.epoch(t0))
    r2, v2 = ast2.eph(kep.epoch(t0 + tof))

    lambert = kep.lambert_problem(r1, r2, tof * kep.DAY2SEC, ast1.mu_central_body)

    vrel_in = tuple(map(lambda x, y: -x + y, lambert.get_v1()[0], v1))
    vrel_out = tuple(map(lambda x, y: -x + y, lambert.get_v2()[0], v2))

    dv_lambert = np.linalg.norm(vrel_out) + np.linalg.norm(vrel_in)

    a, _, _, dv_damon = kep.damon(vrel_in, vrel_out, tof*kep.DAY2SEC)
    m_star = kep.max_start_mass(np.linalg.norm(a), dv_damon, T_max, Isp)
    
    return dv_lambert, dv_damon, m_star
Exemplo n.º 3
0
def lambert_leg(P1, P2, i, j, t1, t2, tof):
    
    ast1 = ASTEROIDS[P1]
    ast2 = ASTEROIDS[P2]

    r1 = state_asteroids.EPH[i][t1][0]
    v1 = state_asteroids.EPH[i][t1][1]
    r2 = state_asteroids.EPH[j][t2][0]
    v2 = state_asteroids.EPH[j][t2][1]

    lambert = kep.lambert_problem(r1, r2, tof * kep.DAY2SEC, ast1.mu_central_body)

    vrel_in = tuple(map(lambda x, y: -x + y, lambert.get_v1()[0], v1))
    vrel_out = tuple(map(lambda x, y: -x + y, lambert.get_v2()[0], v2))

    dv_lambert = np.linalg.norm(vrel_out) + np.linalg.norm(vrel_in)

    a, _, _, dv_damon = kep.damon(vrel_in, vrel_out, tof*kep.DAY2SEC)
    m_star = kep.max_start_mass(np.linalg.norm(a), dv_damon, T_max, Isp)
    
    return dv_lambert, dv_damon, m_star