Project 3: A differential equations model of a Glider
Due Wednesday, 13 November
As we have discussed in class, the flight of a balsa wood glider can be approximately described by the system
where v>0 is the speed of the glider, and is the angle the nose
makes with the horizontal. The
and
terms
represent the effects of gravity, and the
and
account for drag
and lift, respectively. The parameter R adjusts the strength of the drag
on the plane due to air resistance. For most of this project, we will
assume R=0.1.
One of our goals is to answer the following specific questions:
Is it possible to arrange it so that the glider ``lands gently'' instead of crashing? (That is, so that when the height is 0, the glider is approximately horizontal.) If it isn't possible, give a justification. (This question is a bit harder than the others, and is semi-optional. I would like you to at least try, however.)
In addition to answering the above questions, a general description of
what kinds of behaviours can be obtained for all initial conditions
should be presented. Specifically, this means produce a good picture
of the phase plane (the vs. v plane) including several
representative trajectories, explain the different types of
trajectories one can see and how they relate to different types of
glider flight, and illustrate them with graphs of the corresponding
glider's flight (in x vs h coordinates). I suspect that your
write-up would make more sense if you do this part first, and then
answer the specific questions. But that choice is up to you.
You might also want to compare what happens to the types of solutions
when we change R. Are the types of glider flight dramatically
different if R=0.5? How about if R=2? What happens for R=0?
This last part is optional, but I encourage you to try it if you have
time and interest.