Abstract: Systems and methods to deliver crew, cargo and other logistics services to space platforms. In one embodiment, a rendezvous and docking vehicle (RDV) comprises two docking mechanisms coupled to the RDV body. A pressurizable passageway connects the docking mechanisms. In one embodiment, the two docking mechanisms are different. An alternative embodiment comprises docking mechanisms which are the same. Also included is a flight control system. The flight control system may vary between embodiments, being autonomous, automated, or remotely controlled (e.g., remote pilot). One embodiment can also include a docking control system in the RDV. A propulsion system is coupled to the RDV in some embodiments, and the RDV may be augmented by a mated spacecraft's propulsion system in other embodiments. The mated spacecraft's propulsion system may even be under the control of the RDV.

Abstract: Systems and methods for calibrating a LIDAR unit. In one embodiment, a system includes a light pulse detection unit, a delay unit and a two-dimensional target. The light pulse detection unit receives a light pulse from the LIDAR unit. The delay unit produces one or more delayed light pulses which are delayed by a known interval from the light pulse received from the LIDAR unit. The delayed light pulses are used to illuminate the target. Target illumination from each of the delayed light pulses returns to the LIDAR unit with a corresponding known delay. The delay of each delayed light pulse simulates a range that is greater than the actual physical distance from the LIDAR unit to the target. The delay of the light pulses from different parts of the target may be different to simulate different ranges for the different parts of the target.