首页> 外文会议>SPIE Astronomical Telescopes + Instrumentation Conference >Design of the Didymos Reconnaissance and Asteroid Camera for OpNav (DRACO) on the Double Asteroid Redirection Test (DART)
【24h】

Design of the Didymos Reconnaissance and Asteroid Camera for OpNav (DRACO) on the Double Asteroid Redirection Test (DART)

机译:双小行星重定向测试(DART)上用于OpNav的Didymos侦察和小行星相机的设计(DRACO)

获取原文

摘要

The Double Asteroid Redirection Test (DART) is a spacecraft that will impact the smaller body of the binary asteroid Didymos. As a technology demonstration, this will be the first time a kinetic impactor is used to perturb the motion of a near earth object. This technique could someday be used to deflect a dangerous asteroid on a future collision course with Earth. As the only instrument aboard DART, the Didymos Reconnaissance and Asteroid Camera for OpNav (DRACO) serves two purposes. First, DRACO provides images to the Small-body Maneuvering Autonomous Real-Time Navigation (SMARTNav) algorithm, allowing the spacecraft to precisely locate and impact the target. In its final moments, DRACO will also characterize the impact site by providing high resolution, scientific imagery of the surface. Derived from the Long Range Reconnaissance Imager (LORRI) on New Horizons, the telescope is a 208 mm aperture, f/12.6, catadioptric Ritchey-Chretien, with a 0.29 degree field of view. A lightweight opto-mechanical structure, with low CTE mirror substrates and a composite baffle tube, maintains telescope focus in the low temperature environment of deep space. At the focal plane is a 2560 by 2160 pixel, panchromatic, front-side illuminated complementary metal oxide semiconductor (CMOS) image sensor, with digital output, global shutter, and low read noise. A highly integrated focal plane electronics (FPE) module controls the sensor and relays data to the spacecraft.
机译:双小行星重定向测试(DART)是一架太空船,它将撞击双小行星Didymos的较小主体。作为技术演示,这将是动冲击器首次用于扰动近地物体的运动。将来有一天,这种技术可以用来偏转危险的小行星,使其与地球相撞。作为DART上唯一的仪器,Didymos Reconnaissance和OpNav小行星相机(DRACO)有两个用途。首先,DRACO为小型机动自动实时导航(SMARTNav)算法提供图像,使航天器能够精确定位并撞击目标。在最后的时刻,DRACO还通过提供高分辨率,科学的表面图像来表征撞击部位。该望远镜源自“新视野”号的远程侦察成像仪(LORRI),其孔径为208毫米,f / 12.6,折反射里奇-克雷蒂安(Ritchey-Chretien),视野为0.29度。轻巧的光机械结构,具有低CTE镜面基板和复合挡板管,可在深空的低温环境中保持望远镜聚焦。焦平面上是一个2560 x 2160像素的全色正面照明互补金属氧化物半导体(CMOS)图像传感器,具有数字输出,全局快门和低读取噪声。高度集成的焦平面电子设备(FPE)模块控制传感器并将数据中继到航天器。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号