The problem is the following:

- let's say we have a miniaturized satellite*, X;

- we know its position, velocity, acceleration, the forces applied at

any given moment;

- we also know its mass, its dimensions etc;

- the satellite tries to approach a point in space, let's say A(x, y, z).

The question is: what forces (xf, yf, zf) should we apply to our

satellite at any moment, such that the satellite reaches and stops at

point A.

(*) A satellite is a SPHERES (https://en.wikipedia.org/wiki/SPHERES). We don't need to worry about gravitaty. The satellites move by ejecting CO2.

**Edited by valak, 08 December 2018 - 04:04 AM.**