Author_Institution :
Draper (C.S.) Lab., Cambridge, MA, USA
Abstract :
In the early 1930´s, visionary engineers and scientists began thinking about practical self-contained systems for the guidance, navigation, and control of aerospace vehicles in inertial space. Starting with the development of the first gyro compass in 1908, this technology was perfected in the race for improved intercontinental ballistic missile accuracy. Since the end of the cold war, the technology has continued to advance with a focus on systems of lower size, weight and power for a given accuracy. Future systems promise to revolutionize guidance, navigation, and control, with complete low cost inertial measurement units as small as 0.03 cubic inches. This paper reviews the history of the innovations and achievements in inertial guidance technology in the 20th century, and projects the possibilities into the 21st century. The development of inertial guidance technology is traced from its birth to its current broad base application status in aircraft, strategic missiles, satellites, and undersea vehicles
Keywords :
aircraft navigation; gyroscopes; inertial navigation; missile guidance; reviews; technological forecasting; INS/GPS implementation; aerospace control; aerospace vehicles; dynamically tuned two-DOF gyro; fiber optic gyros; gyro compass; gyro-stabilized gun; inertial gimbal system; inertial guidance technology; inertial navigation technology; innovations; intercontinental ballistic missile accuracy; low cost inertial measurement units; micromechanical instruments; miniature electronics; missile guidance; next generation systems; pendulous integrating gyro accelerometer; satellites; self-contained systems; single-DOF integrating rate gyro; strapdown implementation; strategic missiles; undersea vehicle; Aerospace control; Aerospace engineering; Automotive engineering; Control systems; Costs; Inertial navigation; Measurement units; Missiles; Space technology; Space vehicles;