The Mission Operations Team

K. Capelle

The ATV Mission Operations Team works at ATV-CC and comprises a mixed ESA-CNES team. Experienced ESA operations and ground controllers work as Mission Directors and in training, simulation and flight dynamics, while CNES operations engineers work under the CNES Flight Director in areas such as attitude and orbit control, propulsion and telecommunications. ESA's lead Mission Director is Kris Capelle.

Beginning in 2009 with ATV-2, an industrial consortium - referred to as the IOT (Industrial Operations Team) - has been working closely with, and conducting operations for, the ESA-CNES team.

Other teams at the CNES centre in Toulouse support ATV operations in the areas of flight dynamics, training, systems engineering and software development and maintenance.

Mission operations overview

The docking port on the Integrated Cargo Carrier of ATV Johannes Kepler, May 2009

Since ATV will approach and be attached to the ISS, safety is paramount. Most spacecraft functions are doubly redundant, meaning that each subsystem, unit, switch and valve is duplicated - so that the spacecraft can withstand any single failure.

Since anything associated with the ISS must be designed to be triply redundant, ATV is designed to cope with two simultaneous failures.

For example, the ATV propulsion system has both main and redundant thrusters to power it during docking with the ISS. In case both the main and redundant thrusters fail, it has a completely separate, alternative thruster system, controlled by completely different hardware and software.

This system is used particularly if it appears that ATV is not going to dock properly with the ISS. If anything goes wrong, an 'Escape' or a 'Collision Avoidance Manoeuvre' (CAM) can be commanded by ground controllers, by astronauts on the ISS or by the ATV itself, acting autonomously. During an Escape, the normal thrusters are used to bring ATV away from the ISS into a safe parking orbit; during a CAM, the backup thruster system does essentially the same thing.

Much of the complexity of the first ATV mission came from proving that these Escapes and CAMs worked correctly. Only when all of these vital safety operations had been tested, during a 3-week flight campaign, and proven to work flawlessly, was ATV-2 allowed to dock with the ISS. This time ATV-2 will go directly to Station.

Launch and LEOP

The mission starts with the Launch and Early Orbit Phase (LEOP), when the spacecraft is put into a low Earth orbit by Ariane 5. This is probably the most risky part of the mission, especially until ATV has deployed its four solar array panels used to generate the power necessary to control the spacecraft.

After LEOP, the spacecraft performs a series of manoeuvres to bring its orbit into phase with the ISS, approaching it from behind and slightly below.

Simplified view of ATV docking trajectory (click for larger version)

The approach to the ISS is characterised by a series of way-points and station-keeping manoeuvres, which are numbered from S-1/2 (at about 40km from the ISS and marking the start of proximity operations) to S41 - only 12m from docking.

• When ATV reaches S-1/2 (around 40 km behind and 5 km below the ISS), GPS receivers on ATV and the ISS are used to calculate the relative positions of the two bodies. ATV starts a pre-homing phase, passes through S0 (30 km from the ISS), performs the homing phase and stops at station keeping point S2, located 3.5 km behind and 100 m above the ISS.

• When all checks at S2 are completed, a 'Go' command to proceed to S3 (250m behind ISS) is sent to ATV.

• Further checks are performed at S3, and a switch is made to high-performance sensors for control of the final approach.

• After successful checks at S3, ATV will begin its linear translaion into the next hold point (S4, at 25m from the ISS).

ATV will then proceed to S41 (11m from the ISS) and commence docking under permanebt monitoring by the ISS crew and ATV-CC. ATV docks to the Russian Zarya module.

ATV mission scenario - from launch through to destructive re-entry in the Earth's atmosphere

Attached phase

Once attached, the spacecraft is continually monitored. It carries gases and ISS propellant, which are transferred to the ISS during the attached phase along with up to 1600 kg of experiments, and up to 6340 kg of waste material is loaded for the return journey (see specifications below).

For the mission of ATV-2, no water is being delivered to the ISS as none is needed.

During the attached phase, ATV uses its thrusters to correct and adjust the orbit of the 400-tonne ISS structure and to perform debris avoidance manoeuvres when necessary.

Deorbiting

Once ATV undocks from the ISS, it conducts a series of deorbit burns which will cause the vessel to plunge to a fiery end in the upper atmosphere.