Stereophotogrammetric surveying and evaluation method

Claim 1

In a stereophotogrammetric surveying and evaluation method to obtain orientation data of a camera flying over a terrain, and a digital terrain altitude (elevation) model, which camera is not attitude controlled and is especially carried by an aircraft, said camera comprising three sensor lines A, B, C, arranged transversely or obliquely to the flight direction in the image plane of the camera for continuous line by line scanning of the terrain flown over, and generation of overlapping line image strips A S , B S , C S , taken always from a different perspective, the line images each consisting of a plurality of adjacent image points, the improvement comprising that (a) all three line sensors are always used and thereby three overlapping line image strips A S , B S , C S are generated, (b) the line image generation of the sensor lines A, B, C is synchronized and the consecutive numbers N of the line images are registered, (c) in one of the line image strips image points, arranged mesh-like and corresponding to the points of the digital terrain altitude (elevation) model are selected and the corresponding (homologous) image points and their image coordinates x, y and the associated line image numbers N A , N B , N C are determined by means of area correlation in the two other image strips, (d) due to the approximately known flight movements for each digital altitude (elevation) model point with its associated line image numbers N A , N B , N C , the approximate orientation parameters of said camera and from that and with the image point coordinates x A , y A and x B , y B and x C , y C , the digital altitude model coordinates X, Y Z are approximately determined by means of spatial intersection, (e) the establishment of beam intersection conditions for image point beams, belonging to each digital altitude (elevation) model point, takes place, which image point beams are defined by the digital altitude model point, the positions of the perspective center of said camera corresponding to the line image numbers N A , N B , N C , and the image points, located on the sensor lines A, B, C, with the respective x and y coordinates, wherein the orientation parameters are represented as functions of update points which are arranged in certain intervals along the flight path, that error equations are established according to indirect observations, and that the most probable and final values of the orientation parameters in the update points and the digital altitude (elevation) model coordinates are determined by means of a least-squares adjustment process.