A position detector displays a target on a given plane and adds a standard on the given plane in the vicinity of the target with the location of the standard known. An image of the given plane is formed on an image plane of an image sensor with an image of the standard included, a point in the image of the given plane which is formed at a predetermined position of the image plane corresponding to the point to be detected. An image processor identifies the image of the standard on the image plane...

A system is disclosed for using camera attitude sensors with a camera. A camera assembly includes a tripod base, a tripod head interface mounted on the tripod base, a tripod head mounted on the tripod head interface and a camera mounted on the tripod head. The tripod head enables the camera to pan and tilt. The system also includes a first optical encoder for detecting the amount that the camera has been panned and a second optical encoder for detecting the amount that the camera has been tilted...

Methods and structures are provided for reducing pointing errors .zeta. of satellite antennas and for generating broad field-of-view satellite attitude acquisition patterns. In one method embodiment, satellite transmit beams have estimated pointing attitudes .beta. and are transmitted to overlap on a ground-based receiving terminal which has a known terminal location .lambda. and which measures received signal strengths .alpha.. Pointing errors .zeta. of the transmit beams are then determined fr...

A method of comparing a two-dimensional image of an object to library images of that object as seen from a variety of predetermined orientations. The method further includes a rating of the accuracy of fit of the object image to each library image to determining the overall best fit and, thus, the orientation of the object.

An attitude adjustment device for use with a detector device which is used to detect rotational motion about an axis of a unit in which the attitude adjustment device is disposed. The attitude adjustment device includes, but is not limited to, a first adjustment mechanism to adjust the angle of the detector device such that the above-mentioned axis is parallel to a standard axis and is parallel to a first plane. Also, the attitude adjustment device includes a second adjustment mechanism to adjus...

An attitude sensing safing system for a missile, which senses an attitude ror of the missile, and activates a dudding signal when the error exceeds a certain value for a predetermined time. The missile includes a delay arming timer, which is deactivated when by the dudding signal. The system allows the missile to correct itself, by requiring that the error signals persist for a set time.

A method for use in vehicle attitude determination includes generating GPS attitude solutions for a vehicle using three or more antennas receiving GPS signals from two or more space vehicles. An inertial navigation system is initialized by setting the attitude of the inertial navigation system to a GPS attitude solution generated for the vehicle and/or the attitude of the inertial navigation system is updated using the GPS attitude solutions generated for the vehicle or GPS estimated attitude er...

A gravity responsive attitude switch containing electrical contacts separated by a gap, the switch containing a bead liquid and a carrier liquid, the two liquids being immiscible and having different electric resistivity values, where the liquid bead may be disposed between the contacts by properly positioning the switch. The contacts are connected in an electronic circuit which senses the difference in resistivity dependent on whether the bead liquid or the carrier liquid is bridging the gap be...

The present invention provides methods of and apparatus for determining the inertial attitude of an aerospace vehicle. In one embodiment, the invention provides a rotational astronomical object-sighting concept to determine the inertial attitude of an axis of the aerospace vehicle without the star identification or dragback. In another embodiment, the invention provides an attitude measurement apparatus comprising a high sensitivity optical sensor and a low power inertial sensor.

In a vehicle including a stick cylinder movable to change the attitude of a stick relative to a boom, and an implement cylinder movable to change the inclination of an implement relative to the stick, hydraulic circuit means are provided for serially connecting the cylinders so that as the stick cylinder moves the stick in one direction, discharge of fluid from the stick cylinder is used to actuate the implement cylinder to maintain substantially the same attitude of the implement relative to th...