An automatic 
celestial navigation system for navigating both night and day by observation of K-band or H-band 
infrared light from multiple 
stars. In a first set of preferred embodiments three relatively 
large aperture telescopes are rigidly mounted on a movable platform such as a ship or 
airplane with each 
telescope being directed at a substantially different portion of 
sky. Embodiments in this first set tend to be relatively large and heavy, such as about one cubic meter and about 60 pounds. In a second set of preferred embodiments one or more smaller aperture telescopes are pivotably mounted on a movable platform such as a ship, 
airplane or 
missile so that the 
telescope or telescopes can be pivoted to point toward specific regions of the 
sky. Embodiments of this second set are mechanically more complicated than those of the first set, but are much smaller and lighter and are especially useful for guidance of aircraft and missiles. 
Telescope optics focus (on to a 
pixel array of a sensor) H-band or K-band light from one or more 
stars in the 
field of view of each 
telescope. Each 
system also includes an 
inclinometer, an accurate timing device and a computer processor having access to catalogued 
infrared star charts. The processor for each 
system is programmed with special algorithms to use image data from the 
infrared sensors, inclination information from the 
inclinometer, 
time information from the timing device and the catalogued star charts information to determine positions of the platform. 
Direction information from two 
stars is needed for locating the platform with respect to the 
celestial sphere. The computer is also preferably programmed to use this celestial position information to calculate 
latitude and 
longitude which may be displayed on a 
display device such as a monitor or used by a 
guidance control system. These embodiments are jam proof and insensitive to 
radio frequency interference. These systems provide efficient alternatives to GPS when GPS is unavailable and can be used for periodic augmentation of inertial navigation systems.