The Chandra X-ray Observatory is the X-ray component of NASA's Great Observatory Program which includes the recently launched Spitzer Infrared Telescope, the Hubble Space Telescope (HST) for observations in the visible, and the Compton Gamma-Ray Observatory (CGRO) which, after providing years of useful data has reentered the atmosphere. All these facilities provide, or provided, scientific data to the international astronomical community in response to peer-reviewed proposals for their use. The Chandra X-ray Observatory was the result of the efforts of many academic, commercial, and government organizations primarily in the United States but also in Europe. NASA's Marshall Fiducial transfer system (FTS) -directs light from the fiducial lights to the ACA, via a retroreflector collimator (RRC) mounted at the X-ray telescope center, and a periscope.Coarse sun sensor (CSS) -Provides all-sky coverage of the sun. Fine sun sensor (FSS) -Has a 50 o FOV and 0.02 o accuracy. Earth sensor assembly (ESA) -Conical scanning sensor, used during the orbital insertion phase of the mission. Reaction wheel assembly (RWA) -6 momentum wheels which change spacecraft attitude. Momentum unloading propulsion system (MUPS) -Liquid fuel thrusters which allow RWA momentum unloading. Reaction control system (RCS) -Thrusters which change spacecraft attitude. APS Conf. Ser. Style 7ACA The aspect camera assembly ( Figure 6) includes a sunshade (∼2.5 m long, ∼55 cm in diameter), a 11.2 cm, F/9 Ritchey-Chretien optical telescope, and CCD detector(s). This assembly and its related components are mounted on the side of the X-ray telescope. The camera's field of view is 1.4 o × 1.4 o and the sunshade is designed to protect the instrument from the light from the Sun, Earth and Moon, with protection angles of 47 o , 20 o and 6 o , respectively. Only light from the sun can damage the system. Having either the Moon or the Earth in the field-of view only saturates the detector output without incurring damage and therefore only limits the aspects camera's utility. The Moon (Figure 7) 1 has been viewed with Chandra, in part to study the background signal, and in part to learn about the Moon's chemical composition.The aspect camera focal plane detector is a 1024 × 1024 Scientific Imaging Technologies CCD, with 24×24 micron (5×5 ′′ ) pixels, covering the spectral band between 4000 and 9000Å. The CCD is deliberately placed out of focus (point source FWHM = 9 arcsec) to spread the star images over several pixels in order to increase the accuracy of the centering algorithm, and to reduce variation in the point response function over the field of view. There is a spare CCD, which can be illuminated by rotating a mirror.The ACA electronics track a small pixel region (either 4 × 4, 6 × 6, or 8 × 8 pixels) around the fiducial light and star images. There are a total of eight regions available for tracking. Typically five guide stars and three fiducial lights are tracked. The average background is subtracted on-board, and image centroids are calculated by a weighted...