首页> 外文期刊>Icarus: International Journal of Solar System Studies >Noncircular features in Saturn's rings IV: Absolute radius scale and Saturn's pole direction
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Noncircular features in Saturn's rings IV: Absolute radius scale and Saturn's pole direction

机译:土星戒指IV中的非功能特征:绝对半径尺度和土星的杆方向

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We present a comprehensive solution for the geometry of Saturn's ring system, based on orbital fits to an extensive set of occultation observations of 122 individual ring edges and gaps. We begin with a restricted set of very high quality Cassini VIMS, UVIS, and RSS measurements for quasi-circular features in the C and B rings and the Cassini Division, and then successively add suitably weighted additional Cassini and historical occultation measurements (from Voyager, HST and the widely-observed 28 Sgr occultation of 3 Jul 1989) for additional non-circular features, to derive an absolute radius scale applicable across the entire classical ring system. As part of our adopted solution, we determine first-order corrections to the spacecraft trajectories used to determine the geometry of individual occultation chords. We adopt a simple linear model for Saturn's precession, and our favored solution yields a precession rate on the sky (n) over cap (p) = 0.207 +/- 0.006 '' yr(-1), equivalent to an angular rate of polar motion Omega(p) = 0.451 +/- 0.014 '' yr(-1). The 3% formal uncertainty in the fitted precession rate is approaching the point where it can provide a useful constraint on models of Saturn's interior, although realistic errors are likely to be larger, given the linear approximation of the precession model and possible unmodeled systematic errors in the spacecraft ephemerides. Our results are largely consistent with independent estimates of the precession rate based on historical RPX times (Nicholson et al., 1999 AAS/Division for Planetary Sciences Meeting Abstracts #31 31, 44.01) and from theoretical expectations that account for Titan's 700-yr precession period (Vienne and Duriez 1992, Astronomy and Astrophysics 257, 331-352). The fitted precession rate based on Cassini data only is somewhat lower, which may be an indication of unmodeled shorter term contributions to Saturn's polar motion from other satellites, or perhaps the result of inconsistencies in the assumed direction of Saturn's pole in the reconstructed Cassini spacecraft ephemerides. Overall, the agreement of our results with the widely-used French et al. (1993, Icarus 103, 163-214) radius scale is excellent, with very small (less than or similar to 0.1 km) systematic differences, although differences in a few individual feature radii are as large as 6 km. Our new solution incorporates many more features across the ring system, and the fitted orbital elements correct for the several-km biases in the radii of many ring features in the French et al. (1993) catalog that were unresolved because of the large projected diameter of the occulted star in the 28 Sgr event. The formal errors in the fitted radii are generally quite small-on the order of tens of meters. Systematic errors stemming from uncertainty in the precession rate of Saturn's pole and its effect on the accuracy of the reconstructed Cassini trajectories are somewhat larger, but the absolute radius scale is relatively insensitive to 5-sigma changes in the pole direction or precession rate, and we estimate the combined magnitude of these systematic errors and pole uncertainties to be of order 250 m. This estimate is likely to be improved once a new set of reconstructed Cassini trajectories has been developed, based on a self-consistent model for Saturn's pole. We demonstrate the utility of the new radius scale and the associated trajectory corrections in the analysis of short-wavelength density waves in the C ring.
机译:我们为土星环系统的几何形状提供了全面的解决方案,基于轨道拟合到122个单独的环边缘和间隙的广泛掩护观察。我们从一套限制的非常高质量的Cassini Vims,UVIS和RSS测量开始,用于C和B环和Cassini部门的准圆形特征,然后连续增加加权额外的Cassini和历史掩星测量(来自Voyager, HST和1989年7月3日的38 SGR掩星为额外的非圆形特征,导出适用于整个古典环系统的绝对半径尺度。作为我们采用解决方案的一部分,我们将一级校正确定为用于确定各个综合和弦和弦的几何形状的航天器轨迹。我们采用了一个简单的Linear模型,用于土星的PREAPIES,我们的青睐率在天空(N)上产生了一种预示率(P)= 0.207 +/- 0.006'Yr(-1),相当于极性的角速率Motion Omega(P)= 0.451 +/- 0.014'Yr(-1)。拟合预算率的3%正式的不确定性正在接近它对土星内部模型提供有用的限制,尽管鉴于进样模型的线性近似和可能的未确定系统错误,但逼真的误差可能更大。航天飞机的间歇术。我们的结果主要与基于历史RPX时期的预防率的独立估计(Nicholson等,1999年,1999年AAS / Discions)的完全估计符合,从理论期望到泰坦700年的预示期间(维也纳和Duriez 1992,天文学和天体物理学257,331-352)。基于Cassini数据的拟合预算率仅较低,这可能是从其他卫星的极地运动的未拼模块的贡献,或者也许在重建的Cassini Spacecraft杂志中假设的土星杆的假设方向不一致的结果。总体而言,我们的结果与广泛使用的法国等人的协议。 (1993年,ICARUS 103,163-214)半径尺度优异,具有非常小(小于或类似于0.1km)的系统差异,尽管少数个别特征半径的差异如6公里。我们的新解决方案包括环系统上的许多功能,并且适用于法国等人的许多环特征中的几km偏差的安装轨道元素。 (1993)目录,由于28 SGR事件中墨西哥星的大型预计直径而未得到解决。装有半径的正式误差通常很小,大约数十米。源于土星杆的进效率的不确定性的系统误差及其对重建的卡西尼轨迹的准确性的影响有些更大,但绝对半径尺度对极方向或预示率的5-sigma变化相对不敏感,我们估计这些系统误差和极点不确定性的综合幅度为150米。一旦已经开发了一种新的重建的Cassini轨迹,基于土星杆的自我一致模型,这一估计可能会得到改善。我们展示了新的半径尺度和相关轨迹校正在C环中的短波长密度波的分析中的效用。

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