Author_Institution :
Sch. of Autom., Huazhong Univ. of Sci. & Technol., Wuhan, China
Abstract :
In lunar landing missions, it is very important to closely estimate the horizontal velocity of a descending spacecraft for achieving a successful and safe lunar landing. The purpose of this paper is to present a novel, vision-aided approach for the accurate, efficient, and robust estimation of such horizontal velocity. Our algorithm processes images from a downward-looking camera, as well as attitude and altitude information from other sensors, to estimate horizontal velocities. During descent, images vary greatly in scale, orientation, and viewpoint. To begin, the scale-invariant feature transform (SIFT) algorithm copes with such shifts, so one is able to use extracted keypoints to establish correspondences between consecutive descent images. Then, matched SIFT keypoints are projected to the level ground plane according to the measurement of the camera state and the central projection imaging collinear equation. A 1-point random sample consensus (RANSAC) algorithm is adopted to remove mismatched keypoints. From each correctly matched keypoint pair, the algorithm derives a hypothesis for the spacecraft displacement relative to lunar ground, since those keypoints represent measurements of the same position on the lunar surface. From the bundle of displacement hypotheses, our algorithm robustly recovers the mode of the sample distribution. This final horizontal displacement estimate of the spacecraft is obtained by using the mean shift method to search for an appropriate answer among these hypotheses. In combination with the time interval between shots, the horizontal velocity is estimated. Additionally, a digital signal processor with field-programmable gate array architecture is also presented to implement velocity estimation in real time. We evaluate the performance of our algorithm based on numerous simulated image sequences and real flight images compared with the descent image motion estimation system approach and an extended Kalman filter monocular simultaneou- localization and mapping method.
Keywords :
Kalman filters; Moon; aerospace computing; digital signal processing chips; entry, descent and landing (spacecraft); estimation theory; field programmable gate arrays; image sequences; motion estimation; nonlinear filters; transforms; velocity measurement; FPGA architectures; RANSAC algorithm; SIFT algorithm; central projection imaging; collinear equation; descent image motion estimation system; digital signal processor; downward looking descent images; downward-looking camera; extended Kalman filter; field-programmable gate array architecture; horizontal displacement; horizontal velocity estimation; image sequences; level ground plane; lunar landing missions; mapping method; mean shift method; monocular simultaneous localization method; random sample consensus algorithm; real flight images; robust estimation; scale-invariant feature transform algorithm; spacecraft displacement; vision-aided approach; Cameras; Estimation; Feature extraction; Moon; Sensors; Signal processing algorithms; Space vehicles;