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With only 1 dimension, you want to get to position X and stop there. you have a maximum acceleration A you can apply yourself; each frame you choose what direction to accelerate.
So if you have a velocity V, and want to stop at position X as fast as possible, how much of your maximum acceleration A do you apply yourself?
(If you are far away, you apply your maximum acceleration, but when you are close, you start braking. So based on your velocity and remaing distance, you need to decide when you begin to brake.)
The governing equation is x = v t + 0.5 a t^2
where x is distance, v is velocity, t is time, and a is acceleration in compatible units.
With no other constraints, in order to minimize your travel time, you will always apply maximum acceleration: Accelerate in the direction of the goal until you are halfway there, then accelerate in the direction of the origin until you stop.
If you have a maximum velocity, accelerate until you reach that maximum velocity, which will happen at some distance X away from the origin. When you are distance X away from the goal, accelerate back toward the origin.
Just dropping in with the answer to a more advanced version of this question I solved lately. You have v_0 at x_0, and want to reach position X, and have velocity V when reaching there. Acceleration is applied each small time step, e.g. 60 times per second.
So using the equation of motion x = v t + 0.5 a t^2, solve it for t with positive/negative acceleration applied, to see how fast one can reach x, regardless of end speed.
Also calculate how long it would take to reach V by applying the positive or negative acceleration. Whichever t is the highest, is the positive or negative acceleration to apply.
This causes objects to smoothly follow pahts such as sin(x), and if they are thrown off, they will elegantly slide back into it.
I'm trying to create a solar system simulation, and I'm having problems trying to figure out initial velocity vectors for random objects I've placed into the simulation.
Assume:
- I'm using Gaussian grav constant, so all my units are AU/Solar Masses/Day
- Using x,y,z for coordinates
- One star, which is fixed at 0,0,0. Quasi-random mass is determined for it
- I place a planet, at a random x,y,z coordinate, and its own quasi-random mass determined.
Before I start the nbody loop (using RK4), I would like the initial velocity of the planet to be such that it has a circular orbit around the star. Other placed planets will, of course, pull on it once the simulation starts, but I want to give it the chance to have a stable orbit...
So, in the end, I need to have an initial velocity vector (x,y,z) for the planet that means it would have a circular orbit around the star after 1 timestep.
Help? I've been beating my head against this for weeks and I don't believe I have any reasonable solution yet...
It is quite simple if you assume that the mass of the star M is much bigger than the total mass of all planets sum(m[i]). This simplifies the problem as it allows you to pin the star to the centre of the coordinate system. Also it is much easier to assume that the motion of all planets is coplanar, which further reduces the dimensionality of the problem to 2D.
First determine the magnitude of the circular orbit velocity given the magnitude of the radius vector r[i] (the radius of the orbit). It only depends on the mass of the star, because of the above mentioned assumption: v[i] = sqrt(mu / r[i]), where mu is the standard gravitational parameter of the star, mu = G * M.
Pick a random orbital phase parameter phi[i] by sampling uniformly from [0, 2*pi). Then the initial position of the planet in Cartesian coordinates is:x[i] = r[i] * cos(phi[i]) y[i] = r[i] * sin(phi[i])
With circular orbits the velocity vector is always perpendicular to the radial vector, i.e. its direction is phi[i] +/- pi/2 (+pi/2 for counter-clockwise (CCW) rotation and -pi/2 for clockwise rotation). Let's take CCW rotation as an example. The Cartesian coordinates of the planet's velocity are:vx[i] = v[i] * cos(phi[i] + pi/2) = -v[i] * sin(phi[i])vy[i] = v[i] * sin(phi[i] + pi/2) = v[i] * cos(phi[i])
This easily extends to coplanar 3D motion by adding z[i] = 0 and vz[i] = 0, but it makes no sense, since there are no forces in the Z direction and hence z[i] and vz[i] would forever stay equal to 0 (i.e. you will be solving for a 2D subspace problem of the full 3D space).
With full 3D simulation where each planet moves in a randomly inclined initial orbit, one can work that way:
This step is equal to step 1 from the 2D case.
You need to pick an initial position on the surface of the unit sphere. See here for examples on how to do that in a uniformly random fashion. Then scale the unit sphere coordinates by the magnitude of r[i].
In the 3D case, instead of two possible perpendicular vectors, there is a whole tangential plane where the planet velocity lies. The tangential plane has its normal vector collinear to the radius vector and dot(r[i], v[i]) = 0 = x[i]*vx[i] + y[i]*vy[i] + z[i]*vz[i]. One could pick any vector that is perpendicular to r[i], for example e1[i] = (-y[i], x[i], 0). This results in a null vector at the poles, so there one could pick e1[i] = (0, -z[i], y[i]) instead. Then another perpendicular vector can be found by taking the cross product of r[i] and e1[i]:e2[i] = r[i] x e1[i] = (r[2]*e1[3]-r[3]*e1[2], r[3]*e1[1]-r[1]*e1[3], r[1]*e1[2]-r[2]*e1[1]). Now e1[i] and e2[i] can be normalised by dividing them by their norms:n1[i] = e1[i] / ||e1[i]||n2[i] = e2[i] / ||e2[i]||where ||a|| = sqrt(dot(a, a)) = sqrt(a.x^2 + a.y^2 + a.z^2). Now that you have an orthogonal vector basis in the tangential plane, you can pick one random angle omega in [0, 2*pi) and compute the velocity vector as v[i] = cos(omega) * n1[i] + sin(omega) * n2[i], or as Cartesian components:vx[i] = cos(omega) * n1[i].x + sin(omega) * n2[i].xvy[i] = cos(omega) * n1[i].y + sin(omega) * n2[i].yvz[i] = cos(omega) * n1[i].z + sin(omega) * n2[i].z.
Note that by construction the basis in step 3 depends on the radius vector, but this does not matter since a random direction (omega) is added.
As to the choice of units, in simulation science we always tend to keep things in natural units, i.e. units where all computed quantities are dimensionless and kept in [0, 1] or at least within 1-2 orders of magnitude and so the full resolution of the limited floating-point representation could be used. If you take the star mass to be in units of Solar mass, distances to be in AUs and time to be in years, then for an Earth-like planet at 1 AU around a Sun-like star, the magnitude of the orbital velocity would be 2*pi (AU/yr) and the magnitude of the radius vector would be 1 (AU).
Just let centripetal acceleration equal gravitational acceleration.
m1v2 / r = G m1m2 / r2
v = sqrt( G m2 / r )
Of course the star mass m2 must be much greater than the planet mass m1 or you don't really have a one-body problem.
Units are a pain in the butt when setting up physics problems. I've spent days resolving errors in seconds vs timestep units. Your choice of AU/Solar Masses/Day is utterly insane. Fix that before anything else.
And, keep in mind that computers have inherently limited precision. An nbody simulation accumulates integration error, so after a million or a billion steps you will certainly not have a circle, regardless of the step duration. I don't know much about that math, but I think stable n-body systems keep themselves stable by resonances which absorb minor variations, whether introduced by nearby stars or by the FPU. So the setup might work fine for a stable, 5-body problem but still fail for a 1-body problem.
As Ed suggested, I would use the mks units, rather than some other set of units.
For the initial velocity, I would agree with part of what Ed said, but I would use the vector form of the centripetal acceleration:
m1v2/r r(hat) = G m1 m2 / r2 r(hat)
Set z to 0, and convert from polar coordinates to cartesian coordinates (x,y). Then, you can assign either y or x an initial velocity, and compute what the other variable is to satisfy the circular orbit criteria. This should give you an initial (Vx,Vy) that you can start your nbody problem from. There should also be quite a bit of literature out there on numerical recipes for nbody central force problems.
I'm trying to figure out the most efficient/fast way to add a large number of convex quads (four given x,y points) into an array/list and then to check against those quads if a point is within or on the border of those quads.
I originally tried using ray casting but thought that it was a little overkill since I know that all my polygons will be quads and that they are also all convex.
currently, I am splitting each quad into two triangles that share an edge and then checking if the point is on or in each of those two triangles using their areas.
for example
Triangle ABC and test point P.
if (areaPAB + areaPAC + areaPBC == areaABC) { return true; }
This seems like it may run a little slow since I need to calculate the area of 4 different triangles to run the check and if the first triangle of the quad returns false, I have to get 4 more areas. (I include a bit of an epsilon in the check to make up for floating point errors)
I'm hoping that there is an even faster way that might involve a single check of a point against a quad rather than splitting it into two triangles.
I've attempted to reduce the number of checks by putting the polygon's into an array[,]. When adding a polygon, it checks the minimum and maximum x and y values and then using those, places the same poly into the proper array positions. When checking a point against the available polygons, it retrieves the proper list from the array of lists.
I've been searching through similar questions and I think what I'm using now may be the fastest way to figure out if a point is in a triangle, but I'm hoping that there's a better method to test against a quad that is always convex. Every polygon test I've looked up seems to be testing against a polygon that has many sides or is an irregular shape.
Thanks for taking the time to read my long winded question to what's prolly a simple problem.
I believe that fastest methods are:
1: Find mutual orientation of all vector pairs (DirectedEdge-CheckedPoint) through cross product signs. If all four signs are the same, then point is inside
Addition: for every edge
EV[i] = V[i+1] - V[i], where V[] - vertices in order
PV[i] = P - V[i]
Cross[i] = CrossProduct(EV[i], PV[i]) = EV[i].X * PV[i].Y - EV[i].Y * PV[i].X
Cross[i] value is positive, if point P lies in left semi-plane relatively to i-th edge (V[i] - V[i+1]), and negative otherwise. If all the Cross[] values are positive, then point p is inside the quad, vertices are in counter-clockwise order. f all the Cross[] values are negative, then point p is inside the quad, vertices are in clockwise order. If values have different signs, then point is outside the quad.
If quad set is the same for many point queries, then dmuir suggests to precalculate uniform line equation for every edge. Uniform line equation is a * x + b * y + c = 0. (a, b) is normal vector to edge. This equation has important property: sign of expression
(a * P.x + b * Y + c) determines semi-plane, where point P lies (as for crossproducts)
2: Split quad to 2 triangles and use vector method for each: express CheckedPoint vector in terms of basis vectors.
P = a*V1+b*V2
point is inside when a,b>=0 and their sum <=1
Both methods require about 10-15 additions, 6-10 multiplications and 2-7 comparisons (I don't consider floating point error compensation)
If you could afford to store, with each quad, the equation of each of its edges then you could save a little time over MBo's answer.
For example if you have an inward pointing normal vector N for each edge of the quad, and a constant d (which is N.p for one of the vertcies p on the edge) then a point x is in the quad if and only if N.x >= d for each edge. So thats 2 multiplications, one addition and one comparison per edge, and you'll need to perform up to 4 tests per point.This technique works for any convex polygon.
My question is fairly simple. I have two tetrahedra, each with a current position, a linear speed in space, an angular velocity and a center of mass (center of rotation, actually).
Having this data, I am trying to find a (fast) algorithm which would precisely determine (1) whether they would collide at some point in time, and if it is the case, (2) after how much time they collided and (3) the point of collision.
Most people would solve this by doing triangle-triangle collision detection, but this would waste a few CPU cycles on redundant operations such as checking the same edge of one tetrahedron against the same edge of the other tetrahedron upon checking up different triangles. This only means I'll optimize things a bit. Nothing to worry about.
The problem is that I am not aware of any public CCD (continuous collision detection) triangle-triangle algorithm which takes self-rotation in account.
Therefore, I need an algorithm which would be inputted the following data:
vertex data for three triangles
position and center of rotation/mass
linear velocity and angular velocity
And would output the following:
Whether there is a collision
After how much time the collision occurred
In which point in space the collision occurred
Thanks in advance for your help.
The commonly used discrete collision detection would check the triangles of each shape for collision, over successive discrete points in time. While straightforward to compute, it could miss a fast moving object hitting another one, due to the collision happening between discrete points in time tested.
Continuous collision detection would first compute the volumes traced by each triangle over an infinity of time. For a triangle moving at constant speed and without rotation, this volume could look like a triangular prism. CCD would then check for collision between the volumes, and finally trace back if and at what time the triangles actually shared the same space.
When angular velocity is introduced, the volume traced by each triangle no longer looks like a prism. It might look more like the shape of a screw, like a strand of DNA, or some other non-trivial shapes you might get by rotating a triangle around some arbitrary axis while dragging it linearly. Computing the shape of such volume is no easy feat.
One approach might first compute the sphere that contains an entire tetrahedron when it is rotating at the given angular velocity vector, if it was not moving linearly. You can compute a rotation circle for each vertex, and derive the sphere from that. Given a sphere, we can now approximate the extruded CCD volume as a cylinder with the radius of the sphere and progressing along the linear velocity vector. Finding collisions of such cylinders gets us a first approximation for an area to search for collisions in.
A second, complementary approach might attempt to approximate the actual volume traced by each triangle by breaking it down into small, almost-prismatic sub-volumes. It would take the triangle positions at two increments of time, and add surfaces generated by tracing the triangle vertices at those moments. It's an approximation because it connects a straight line rather than an actual curve. For the approximation to avoid gross errors, the duration between each successive moments needs to be short enough such that the triangle only completes a small fraction of a rotation. The duration can be derived from the angular velocity.
The second approach creates many more polygons! You can use the first approach to limit the search volume, and then use the second to get higher precision.
If you're solving this for a game engine, you might find the precision of above sufficient (I would still shudder at the computational cost). If, rather, you're writing a CAD program or working on your thesis, you might find it less than satisfying. In the latter case, you might want to refine the second approach, perhaps by a better geometric description of the volume occupied by a turning, moving triangle -- when limited to a small turn angle.
I have spent quite a lot of time wondering about geometry problems like this one, and it seems like accurate solutions, despite their simple statements, are way too complicated to be practical, even for analogous 2D cases.
But intuitively I see that such solutions do exist when you consider linear translation velocities and linear angular velocities. Don't think you'll find the answer on the web or in any book because what we're talking about here are special, yet complex, cases. An iterative solution is probably what you want anyway -- the rest of the world is satisfied with those, so why shouldn't you be?
If you were trying to collide non-rotating tetrahedra, I'd suggest a taking the Minkowski sum and performing a ray check, but that won't work with rotation.
The best I can come up with is to perform swept-sphere collision using their bounding spheres to give you a range of times to check using bisection or what-have-you.
Here's an outline of a closed-form mathematical approach. Each element of this will be easy to express individually, and the final combination of these would be a closed form expression if one could ever write it out:
1) The equation of motion for each point of the tetrahedra is fairly simple in it's own coordinate system. The motion of the center of mass (CM) will just move smoothly along a straight line and the corner points will rotate around an axis through the CM, assumed to be the z-axis here, so the equation for each corner point (parameterized by time, t) is p = vt + x + r(sin(wt+s)i + cos(wt + s)j ), where v is the vector velocity of the center of mass; r is the radius of the projection onto the x-y plane; i, j, and k are the x, y and z unit vectors; and x and s account for the starting position and phase of rotation at t=0.
2) Note that each object has it's own coordinate system to easily represent the motion, but to compare them you'll need to rotate each into a common coordinate system, which may as well be the coordinate system of the screen. (Note though that the different coordinate systems are fixed in space and not traveling with the tetrahedra.) So determine the rotation matrices and apply them to each trajectory (i.e. the points and CM of each of the tetrahedra).
3) Now you have an equation for each trajectory all within the same coordinate system and you need to find the times of the intersections. This can be found by testing whether any of the line segments from the points to the CM of a tetrahedron intersects the any of the triangles of another. This also has a closed-form expression, as can be found here.
Layering these steps will make for terribly ugly equations, but it wouldn't be hard to solve them computationally (although with the rotation of the tetrahedra you need to be sure not to get stuck in a local minimum). Another option might be to plug it into something like Mathematica to do the cranking for you. (Not all problems have easy answers.)
Sorry I'm not a math boff and have no idea what the correct terminology is. Hope my poor terms don't hide my meaning too much.
Pick some arbitrary timestep.
Compute the bounds of each shape in two dimensions perpendicular to the axis it is moving on for the timestep.
For a timestep:
If the shaft of those bounds for any two objects intersect, half timestep and start recurse in.
A kind of binary search of increasingly fine precision to discover the point at which a finite intersection occurs.
Your problem can be cast into a linear programming problem and solved exactly.
First, suppose (p0,p1,p2,p3) are the vertexes at time t0, and (q0,q1,q2,q3) are the vertexes at time t1 for the first tetrahedron, then in 4d space-time, they fill the following 4d closed volume
V = { (r,t) | (r,t) = a0 (p0,t0) + … + a3 (p3,t0) + b0 (q0,t1) + … + b3 (q3,t1) }
Here the a0...a3 and b0…b3 parameters are in the interval [0,1] and sum to 1:
a0+a1+a2+a3+b0+b1+b2+b3=1
The second tetrahedron is similarly a convex polygon (add a ‘ to everything above to define V’ the 4d volume for that moving tetrahedron.
Now the intersection of two convex polygon is a convex polygon. The first time this happens would satisfy the following linear programming problem:
If (p0,p1,p2,p3) moves to (q0,q1,q2,q3)
and (p0’,p1’,p2’,p3’) moves to (q0’,q1’,q2’,q3’)
then the first time of intersection happens at points/times (r,t):
Minimize t0*(a0+a1+a2+a3)+t1*(b0+b1+b2+b3) subject to
0 <= ak <=1, 0<=bk <=1, 0 <= ak’ <=1, 0<=bk’ <=1, k=0..4
a0*(p0,t0) + … + a3*(p3,t0) + b0*(q0,t1) + … + b3*(q3,t1)
= a0’*(p0’,t0) + … + a3’*(p3’,t0) + b0’*(q0’,t1) + … + b3’*(q3’,t1)
The last is actually 4 equations, one for each dimension of (r,t).
This is a total of 20 linear constraints of the 16 values ak,bk,ak', and bk'.
If there is a solution, then
(r,t)= a0*(p0,t0) + … + a3*(p3,t0) + b0*(q0,t1) + … + b3*(q3,t1)
Is a point of first intersection. Otherwise they do not intersect.
Thought about this in the past but lost interest... The best way to go about solving it would be to abstract out one object.
Make a coordinate system where the first tetrahedron is the center (barycentric coords or a skewed system with one point as the origin) and abstract out the rotation by making the other tetrahedron rotate around the center. This should give you parametric equations if you make the rotation times time.
Add the movement of the center of mass towards the first and its spin and you have a set of equations for movement relative to the first (distance).
Solve for t where the distance equals zero.
Obviously with this method the more effects you add (like wind resistance) the messier the equations get buts its still probably the simplest (almost every other collision technique uses this method of abstraction). The biggest problem is if you add any effects that have feedback with no analytical solution the whole equation becomes unsolvable.
Note: If you go the route of of a skewed system watch out for pitfalls with distance. You must be in the right octant! This method favors vectors and quaternions though, while the barycentric coords favors matrices. So pick whichever your system uses most effectively.
I've tried the typical physics equations for this but none of them really work because the equations deal with constant acceleration and mine will need to change to work correctly. Basically I have a car that can be going at a large range of speeds and needs to slow down and stop over a given distance and time as it reaches the end of its path.
So, I have:
V0, or the current speed
Vf, or the speed I want to reach (typically 0)
t, or the amount of time I want to take to reach the end of my path
d, or the distance I want to go as I change from V0 to Vf
I want to calculate
a, or the acceleration needed to go from V0 to Vf
The reason this becomes a programming-specific question is because a needs to be recalculated every single timestep as the car keeps stopping. So, V0 constantly is changed to be V0 from last timestep plus the a that was calculated last timestep. So essentially it will start stopping slowly then will eventually stop more abruptly, sort of like a car in real life.
EDITS:
All right, thanks for the great responses. A lot of what I needed was just some help thinking about this. Let me be more specific now that I've got some more ideas from you all:
I have a car c that is 64 pixels from its destination, so d=64. It is driving at 2 pixels per timestep, where a timestep is 1/60 of a second. I want to find the acceleration a that will bring it to a speed of 0.2 pixels per timestep by the time it has traveled d.
d = 64 //distance
V0 = 2 //initial velocity (in ppt)
Vf = 0.2 //final velocity (in ppt)
Also because this happens in a game loop, a variable delta is passed through to each action, which is the multiple of 1/60s that the last timestep took. In other words, if it took 1/60s, then delta is 1.0, if it took 1/30s, then delta is 0.5. Before acceleration is actually applied, it is multiplied by this delta value. Similarly, before the car moves again its velocity is multiplied by the delta value. This is pretty standard stuff, but it might be what is causing problems with my calculations.
Linear acceleration a for a distance d going from a starting speed Vi to a final speed Vf:
a = (Vf*Vf - Vi*Vi)/(2 * d)
EDIT:
After your edit, let me try and gauge what you need...
If you take this formula and insert your numbers, you get a constant acceleration of -0,0309375. Now, let's keep calling this result 'a'.
What you need between timestamps (frames?) is not actually the acceleration, but new location of the vehicle, right? So you use the following formula:
Sd = Vi * t + 0.5 * t * t * a
where Sd is the current distance from the start position at current frame/moment/sum_of_deltas, Vi is the starting speed, and t is the time since the start.
With this, your decceleration is constant, but even if it is linear, your speed will accomodate to your constraints.
If you want a non-linear decceleration, you could find some non-linear interpolation method, and interpolate not acceleration, but simply position between two points.
location = non_linear_function(time);
The four constraints you give are one too many for a linear system (one with constant acceleration), where any three of the variables would suffice to compute the acceleration and thereby determine the fourth variables. However, the system is way under-specified for a completely general nonlinear system -- there may be uncountably infinite ways to change acceleration over time while satisfying all the constraints as given. Can you perhaps specify better along what kind of curve acceleration should change over time?
Using 0 index to mean "at the start", 1 to mean "at the end", and D for Delta to mean "variation", given a linearly changing acceleration
a(t) = a0 + t * (a1-a0)/Dt
where a0 and a1 are the two parameters we want to compute to satisfy all the various constraints, I compute (if there's been no misstep, as I did it all by hand):
DV = Dt * (a0+a1)/2
Ds = Dt * (V0 + ((a1-a0)/6 + a0/2) * Dt)
Given DV, Dt and Ds are all given, this leaves 2 linear equations in the unknowns a0 and a1 so you can solve for these (but I'm leaving things in this form to make it easier to double check on my derivations!!!).
If you're applying the proper formulas at every step to compute changes in space and velocity, it should make no difference whether you compute a0 and a1 once and for all or recompute them at every step based on the remaining Dt, Ds and DV.
If you're trying to simulate a time-dependent acceleration in your equations, it just means that you should assume that. You have to integrate F = ma along with the acceleration equations, that's all. If acceleration isn't constant, you just have to solve a system of equations instead of just one.
So now it's really three vector equations that you have to integrate simultaneously: one for each component of displacement, velocity, and acceleration, or nine equations in total. The force as a function of time will be an input for your problem.
If you're assuming 1D motion you're down to three simultaneous equations. The ones for velocity and displacement are both pretty easy.
In real life, a car's stopping ability depends on the pressure on the brake pedal, any engine braking that's going on, surface conditions, and such: also, there's that "grab" at the end when the car really stops. Modeling that is complicated, and you're unlikely to find good answers on a programming website. Find some automotive engineers.
Aside from that, I don't know what you're asking for. Are you trying to determine a braking schedule? As in there's a certain amount of deceleration while coasting, and then applying the brake? In real driving, the time is not usually considered in these maneuvers, but rather the distance.
As far as I can tell, your problem is that you aren't asking for anything specific, which suggests that you really haven't figured out what you actually want. If you'd provide a sample use for this, we could probably help you. As it is, you've provided the bare bones of a problem that is either overdetermined or way underconstrained, and there's really nothing we can do with that.
if you need to go from 10m/s to 0m/s in 1m with linear acceleration you need 2 equations.
first find the time (t) it takes to stop.
v0 = initial velocity
vf = final velocity
x0 = initial displacement
xf = final displacement
a = constant linear acceleration
(xf-x0)=.5*(v0-vf)*t
t=2*(xf-x0)/(v0-vf)
t=2*(1m-0m)/(10m/s-0m/s)
t=.2seconds
next to calculate the linear acceleration between x0 & xf
(xf-x0)=(v0-vf)*t+.5*a*t^2
(1m-0m)=(10m/s-0m/s)*(.2s)+.5*a*((.2s)^2)
1m=(10m/s)*(.2s)+.5*a*(.04s^2)
1m=2m+a*(.02s^2)
-1m=a*(.02s^2)
a=-1m/(.02s^2)
a=-50m/s^2
in terms of gravity (g's)
a=(-50m/s^2)/(9.8m/s^2)
a=5.1g over the .2 seconds from 0m to 10m
Problem is either overconstrained or underconstrained (a is not constant? is there a maximum a?) or ambiguous.
Simplest formula would be a=(Vf-V0)/t
Edit: if time is not constrained, and distance s is constrained, and acceleration is constant, then the relevant formulae are s = (Vf+V0)/2 * t, t=(Vf-V0)/a which simplifies to a = (Vf2 - V02) / (2s).