Similar Items: Autonomous docking for a satellite pair using monocular vision
- Development and verification of an electro-mechanical docking mechanism for flight
- 3D tracking between satellites using monocular computer vision
- A CubeSat docking module prototype
- A hardware-in-the-loop simulation facility for the attitude determination and control system of SUNSAT
- A Bore-sight Motion Detection Algorithm for Satellite Attitude Control
- Feasibility of using an ARM processor in a micro satellite on-board computer
Author: Steyn, W. H.
- The safety and comfort of a patient during robot-based positioning for accurate radiotherapy
- The development of a hardware-in-the-loop platform for the attitude determination and control testing of a small satellite
- A low cost, high precision star sensor
- Spinning solar sail : the deployment and control of a spinning solar sail satellite
- Control moment gyro actuator for small satellite applications
- Development of CubeStar : a CubeSat-compatible star tracker