This paper describes results from a recent helicopter field test of a binocular stereo vision system for deorbit descent and landing applications. The system consisted of two 18.6˚ field of view cameras mounted 1.7m apart. Post processing of the images showed ranging accuracy better than 1% up to 500m and 17 cm/s velocimetry accuracy at 37m. For a flight system these images could be input into an FPGA-based processor which processes dense stereo and visual odometry in less than 1 second to achieve the stereo ranging frame rates required for soft landing. When coupled with vision based Terrain Relative Navigation this stereo system enables landing accuracies on the order of 10m.
Demonstration of stereo vision for deorbit descent and landing
2019-01-31
Preprint
No indication
English
Oft-1 Reference Flight Profile. Deorbit Through Landing
NTIS | 1977
|OFT-1 reference flight profile. Deorbit through landing
NTRS | 1977
|