Since the first orbiting explorations, the rendezvous maneuver has become a fundamental operation in space missions. The operation consists of a spacecraft alignment to a specific target point, usually another spacecraft or some debris orbiting in the space. A successful rendezvous mission usually requires the determination of the trajectory, the speed, and the timing of the approaching spacecraft to ensure a safe and accurate approach. In this work thesis, the rendezvous problem is explained and analysed. Then, a control algorithm that guides an autonomous spacecraft to a requested position close to the target is proposed. Usually a spacecraft during the mission could encounter obstacles along the orbit, such as a meteorite to be dodged along the trajectory.