ABSTRACT

In an issue of Wireless World magazine, back in 1945, A. C. Clarke in a letter to the editor wrote, “However, I would like to close

by mentioning a possibility of the remote future-perhaps half a

century ahead . . . . Three repeater stations, twelve degrees apart

in the correct orbit, could give television and microwave coverage

to the entire planet.” These words envisioned, before the space

era even started, the now overcrowded geostationary orbit, while

also introducing one of the most lucrative commercial applications

of the space business: telecommunications. It is worth noting

in this context, how this early space mission concept made use

of multiple satellites to achieve its goal. Twenty years later, the

space era actually began with the successful launch of the Russian

satellite Sputnik I. In the following years, many missions have

been proposed, designed, and realized that make use of multiple

satellites, probes, planetary rovers, robots, or, in general, what

can be called “space agents” to underline the connection to

multiagent systems research. The European Space Agency (ESA)

mission named Cluster II, currently orbiting around our planet, is

made of four identical satellites that need to accurately fly in a

tetrahedron formation during part of their orbit. This particular

geometry allows for the determination of three-dimensional and

time-varying phenomena related to Earth’s magnetic field. Several

satellite constellations, among which the currently active global

positioning system (GPS), Globastar, and Iridium and also the

planned European Galileo and Swarm constellation are formed

of many identical spacecrafts (up to 50) that achieve a common

overall objective, thanks to complex orbital and communication

strategies. The innovative and ambitious Teledesic project (involving

contributions from Bill Gates and Paul Allen but canceled in 2001)

considered, at a certain point, to employ 840 active identical

satellites orbiting Earth to provide a global Internet service. In the

United States, the National Aeronautics and Space Administration

(NASA) is working on a mission called Terrestrial Planet Finder

(TPF), a mission consisting of five separate spacecrafts working

together to function as one single huge telescope-likewise the

considered ESA science mission named Darwin (see Fig. 18.1).

NASA rovers Spirit and Opportunity are currently performing a

collective exploration of the Martian planetary surface [Squyres

(2005)] while allowing scientists to test sophisticated intelligent

algorithms [Estlin et al. (2007)]. The ESA technology demonstrator Proba 3, currently in its design phase [Borde et al. (2004)], requires two heterogeneous satellites to acquire a quite complex

and coordinated orbital movement with one satellite partially

“shadowing” the second, allowing a solar coronography experiment.

A possible architecture of a human mission to Mars involves an

in-orbit assembly of several heterogeneous components launched

separately (this scenario was touched upon by the Concurrent

Design Facility at the ESA during the early architecture study of the

Human Mission to Mars). These are only a few selected examples

of space missions that need coordination between two or more

satellites to achieve their overall goal and that have been already

developed beyond a purely conceptual design. This last criterion

partitions the set of all the ever-conceived space missions into

quite distinct classes. It is no surprise that interesting missions

belong also to the other class, the one often including concepts far

fetched in the future, concepts that are typically attracting smaller

investments as they currently fail to be economically viable or to

have an appropriate technological readiness level. These include the

homogeneous in-orbit assembly concept, where several identical

spacecrafts assemble a large structure (e.g., a reflective mirror

or a gigantic solar panel made of 861 elements placed in an

hexagonal lattice [Izzo et al. (2005)]); the fractionated spacecraft [Mathieu and Weigel (2005)], where one whole spacecraft is

substituted by independent heterogeneous modules carrying out

specialized functions in coordination; the Japanese Petsat project

[Nakasuka et al. (2006)], where the spacecraft is essentially made of LEGO-type modules that can assemble in different types of

shapes and reconfigure to carry out different tasks; the APIES

mission [D’Arrigo and Santandrea (2003)], employing a swarm of

spacecrafts to collectively explore the asteroid belt; the early NASA

Autonomous NanoTechnology Swarm (ANTS) concept [Curtis et al. (2000)]; and the many concepts on planetary exploration that

involve multiple probes and rovers collectively performing tasks on

planetary surfaces and atmospheres. It is worth to highlight the

work done at the Massachusetts Institute of Technology (MIT) in

the framework of the project named SPHERES, which considers, as an objective, to develop and test sophisticated algorithms to

achieve precise autonomous coordinated movement of three metal

spheres placed in a zero-gravity environment. The three spheres

are built (see Fig. 18.2) and, as of 2006, are functioning onboard

the International Space Station (ISS). A program to upgrade the

hardware with cameras is ongoing, and the SPHERE-Zero-Robotics

initiative will soon provide students with access to a microgravity

environment for experimentation and analysis. A number of papers

[Mohan et al. (2009); Saenz-Otero et al. (2009); Nolet et al. (2007)] published recently report on themost significant advances obtained.