Earth spins about 360 degrees within 24 hours. Therefore

ß = [2p/24) -/+ 2p/(365.25*24) ] * t ; t is the Earth time difference of detecting asteroid at two different moments. And (-/+) depends on the considering direction of revolving Earth around sun.

Let W is the tangential velocity of Earth at point A0 , W’ is the tangential velocity of Earth at point ‘A’ within space time. And U is the velocity of the asteroid with respect to ‘Earth detection’ at the first moment of detection at point A0. i.e. U was the velocity of the asteroid whenever now coming EM waves toward point A0 were emitted. And U’ is similar to the 2nd detection of EM waves at point A. And important : U is the velocity component of V at A0 in the direction A0Y and U’ is also the velocity component of V, at position A, in the direction A0Y.

Then U = V cos(?).cos(?)………………………(1)

U’ = – V’.cosd.cos a.cos ß. (minus include : because asteroid velocity component at the 2nd detection is in the opposite direction of A0Y)

V’ is the velocity of the asteroid with respect to the Earth ,whenever now coming(at the 2nd detection of EM waves coming from the asteroid) EM waves were emitted. We can consider

V’ =k.V k is a complex constant or function of V. Therefore

U’ = -kV.cosd.cos a.cos ß……………………(2)

ß explanation :

We know Earth has two velocity components.

1. Due to axial rotation there is a tangential velocity component at point A0.

2. Due to the revolution around the sun , there is an another velocity component.

Revolution component of velocity W (along the direction A0Y ) = r0*(2p/365.25*24)* cos ?

Where ? = (2p*t1)/24

Explanation :

Angular velocity of Earth to spin about its axis = 2p/T

time taken to rotate the Earth about an angle ? = t1 = time difference between the moment of asteroid 1st detection occurs and the time of the place such that the sun is overhead (whenever 1st detection is occurring) That (t1) can be easily measure: just the time difference between two clocks placed at A0 and sun overhead position.

Similarly revolution component of velocity W’ along the direction A0Y =

r0’ * (2p/365.25*24)*cos ?’ *cos ß

Where r0’ is the distance between sun and Earth whenever the 2nd detection occurs.

And ?’ = (2p*t2/24)

Where t2 is the time difference between the position of 2nd detection occurs and similar sun overhead position.

Tangential velocity component of W = R(2p/24)

Tangential velocity component of W’ = R(2p/24).cos ß

R is the mean radius of the Earth.

Then,

W = [ R(2p/24) + r0*(2p/365.25*24)* cos ? ]…………………(3)

W’ = [ R(2p/24).cos ß + r0’ * (2p/365.25*24)*cos ?’ *cos ß]………………………(4)

We can measure the values of ? and a : By measuring the angle between the flat Earth surface at point A0 and the direction of asteroid observable; we can measure the angle ?. And by measuring the angle between the flat Earth surface at point A and the direction of asteroid observable ; we can directly measure the angle a.

We can measure the intensity of coming EM waves towards the point A0(I1) by using suitable instrument as well as intensities of EM waves coming towards point A( I2 ) We have,

When ? ?0, I1 ? I1,max and when d ?0, I2 ?I2, max. Therefore using the equation of maximum intensity and the intensity equations for point A0 and A, we can calculate the values of ? and d. Then we can get expressions for U and U’ in terms of V. We can directly get the values of Wand W’ as constant values. Let W= k1 and W’ = k2. Then the relative velocity of Earth with respect to the asteroid at position A0= V1 = k1 – g1(V)…………………………(5)

Then the relative velocity of Earth with respect to the asteroid at position A =

V2 = k2– g2(V)…………………………(6)Where g

1(V) is the expression get from equation (1) and g2 (V) is the expression get from the equation (2). Then by relativistic Doppler formula we get

f1 = [ 1/ v(1- (V1/C) ) ]. { 1- (W/U) }. f0

f2 = [ 1/ v(1- (V2/C) ) ]. { 1- (W’/U’) }. f0’

Where f1 is the frequency of coming EM waves toward point A0 detected at point A0. And f2 is similar frequency at point A. And f0 is the real frequency of EM waves coming towards A0, when they were emitting. And f0’ is the real frequency of the EM waves coming towards A, when they were emitting by asteroid. Since time difference between two detection of asteroid is very small , we can consider f0 = f0’ .Therefore by the above equations,

f1 / f2 = [ 1/ v(1- (V1/C) ) ]. { 1- (W/U) } / [ 1/ v(1- (V2/C) ) ]. { 1- (W’/U’) }

Therefore we get the relation that contains V and k(V)terms. Therefore if we assume

k(V) =1( that means velocity of the asteroid does not change within that time interval of two detections occurs ), then we can estimate the value of V.

By substituting that V value to equation (1) we can find value of f1. And after that if we substitute that V value, to equation (2) and we can find value of f2. Then we get the difference of f1 and f2. If f1< f2 ; then we can conclude that that asteroid gradually becomes energize(may not be happened) , if f2< f1 ; then we can conclude that the asteroid gradually becomes weaker in energy.

If we assume f1 = f2 directly, then by substituting that V value to both equations and by comparing those k(V) value with the integer orders of V value we got, we can get rough idea about the function k(V). Then by using some equations in relative motions and etc. we can estimate how far the asteroid from the Earth roughly.