Abstract: In some aspects, the techniques described herein relate to a method including: determining a target in a line of sight of an imaging device mounted to an aircraft; acquiring a plurality of images from the imaging device while steering the aircraft through a trajectory about the target; determining a mapping of a fixed reference feature in the plurality of images; and determining an error in an orientation of the imaging device based upon the mapping of the fixed reference feature.

Abstract: In some aspects, the techniques described herein relate to a method including: determining a target in a line of sight of an imaging device mounted to an aircraft; acquiring a plurality of images from the imaging device while steering the aircraft through a trajectory about the target; determining a mapping of a fixed reference feature in the plurality of images; and determining an error in an orientation of the imaging device based upon the mapping of the fixed reference feature.

Abstract: An active vibration isolation system (10) includes a plurality of stiff actuators, such as piezoelectric motors (12a-c; 284, 350) which support a small mass (18) inside of a case (300). A passive isolator (20) is interposed between the small mass (18) and the payload mass (M.sub.p). In the instance where the stiff actuators are piezoelectric motors, the sidewalls of the case (300) are used to provide compressive force along the variable length of each of the horizontal piezoelectric motor elements (284, 350) to prevent damage to same. Compensation circuitry (24) is connected between velocity sensors (17) and the stiff actuators to control the variable length thereof in this move-out-of-the-way system (10) and to compensate for resonating modes. Optionally, a payload mass velocity sensor (26) and associated circuitry may be used to provide additional control.

Abstract: An active vibration isolation system (10) includes a plurality of stiff actuators, such as piezoelectric motors (12a-c; 284, 350) which support a small mass (18) inside of a case (300). A passive isolator (20) is interposed between the small mass (18) and the payload mass (M.sub.p). In the instance where the stiff actuators are piezoelectric motors, the sidewalls of the case (300) are used to provide compressive force along the variable length of each of the horizontal piezoelectric motor elements (284, 350) to prevent damage to same. Compensation circuitry (24) is connected between velocity sensors (17) and the stiff actuators to control the variable length thereof in this move-out-of-the-way system (10) and to compensate for resonating modes. Optionally, a payload mass velocity sensor (26) and associated circuitry may be used to provide additional control.