- #1

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Hello

Given:

Point A

Body B with angular velocity ω

C body with radius

Spacecraft with constant velocity

We neglect the gravity of the bodies B, C

The problem:

Find the shortest trajectory for spacecraft from A to B

What approaches might be here?

How might the solution be changed if we consider the gravity of C and

Given:

Point A

Body B with angular velocity ω

C body with radius

*r*Spacecraft with constant velocity

*v.*We neglect the gravity of the bodies B, C

The problem:

Find the shortest trajectory for spacecraft from A to B

What approaches might be here?

How might the solution be changed if we consider the gravity of C and

*v*would be initial velocity?