wave - particle duality solution

8/9/2019 Wave - particle duality solution

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Wave particle duality Illusion [email protected]

By professor Joe Nahhas

It is a particle you dummy

All there is in the Universe is objects of mass m moving in space (x, y, z) ata location r = r (x, y, z). The state of any object in the Universe can be

expressed as the product

S = m r; State = mass x location:P = d S/d t = m (d r/d t) + (dm/d t) r = Total moment

= change of location + change of mass= m v + m' r; v = velocity = d r/d t; m' = mass change rate

F = d P/d t = dS/dt = Total force= m (dr/dt) +2(dm/d t) (d r/d t) + (dm/dt) r= m + 2m'v +m" r; = acceleration; m'' = mass acceleration rate
mailto:[email protected]:[email protected]


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In polar coordinates system

r = r r (1) ;v = r' r(1) + r ' (1) ; = (r" - r')r(1) + (2r'' + r ")(1)r = location; v = velocity; = acceleration

F = m + 2m'v +m" rF = m [(r"-r') r (1) + (2r'' + r ") (1)]+2m'[r' r (1) + r ' (1)]+ (m" r) r (1)

= [d (m r)/dt - (m r) '] r (1) + (1/mr) [d (mr')/d t] (1)= 0 Light force law

Proof:First r = r [cosine + sine ] = r r (1)Define r (1) = cosine + sine Define v = d r/d t = r' r (1) + r d[r (1)]/d t = r' r (1) + r'[- sine + cosine ]

= r' r (1) + r ' (1)Define (1) = -sine +cosine ;And with r (1) = cosine + sine

Page 4Then d [ (1)]/d t= ' [- cosine - sine = - ' r (1)And d [r (1)]/d t = ' [-sine + cosine ] = ' (1)Define= d [r' r (1) + r ' (1)] /d t

= r" r (1) + r'd [r (1)]/d t + r' ' r (1) + r " r (1) +r 'd [ (1)]/d t = (r" - r') r (1) + (2r'' + r ") (1)With d (m r)/dt - (m r) ' = F (r)

And d (mr')/d t = 0If light mass m = constant, thenWith d r/dt - r ' = F (r) Eq-1And d (r')/d t = 0 Eq-2With d r/dt - r ' = 0 E q 1And d (r')/d t = 0 Eq-2

From Eq-2: d (r')/d t = 0Then r' = h = constantDifferentiate with respect to time

Then 2rr'' + r" = 0Divide by r'Then 2(r'/r) + "/' = 0And 2(r'/r) = - "/' = 2[ (r) + (r)]Also, r = r0 (, 0) e [ (r) + (r)] t

And ' = ' 0 (, 0) e -2[ (r) + (r)] tFor a fixed orbit: r = 0


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Also, r = r 0 (, 0)e t

And ' = ' 0 (, 0) e -2 tWith d r/dt - r ' = 0Let u = 1/r; r = 1/u; r' = h = /uAnd d r/d t = (d r/ d u) (d u /d ) (d / d t) = (- 1/u ) () (d u/ d )

= - h (d u/ d )And d r/ d t = - h () (d u/ d )

= [- h/r] (d u/ d )= - h u (d u/ d )

With d r/dt - r ' = 0 E q 1And - h u (d u/ d ) (1/u) (h u) = 0Then (d u/ d ) + u = 0Then u = A e - Then r 0 (, 0) = (1/A) e And r 0 (, 0) = r 0 (0, 0) e And r = r 0 (0, 0) e e tOr, r = r 0 e (+ t)

This is real time light motion that Arabs drew in 950 AD

What the Arabs said we see and measure is along the line of sight

A- Arabs real time astronomy:The Arabs Astronomers and Physicists said that:

We can not see detect or measure something in space that did notexist and that had not happened. We can only see detect and measure


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things and events in space that had happened. What we see detectand measure is not what there is and not what happened. We seedetect and measure traces and images of objects of past event. Wesee detect and measure in present time images of object and eventsthat happened in past time. That is we measure images and record

data of objects of past events in present time

Present time = present timePresent time = past time + (present time past time)Present time = past time + time differencePresent time = real time; past time = event time; (present time pasttime) = time delay, or, Real time = event time + time delay

Real time Astronomy = Event time Astronomy + time delaysAstronomyIn Modern Physics language the Arabs would have said

Quantum = classical + relativisticWhat there is = classicalWhat we see and measure detect partially = quantumWhat we see and measure and has no detection = relativisticTime dependent measurements = time independent measurements +(Time dependent measurements time independent measurements)

Measured = actual + (measured actual)We do not see object in real time but we see images of objects in real time

In common Terms: Image = object + (image object)

With Image = I; object = OI = O + (I O)I/O = O/O + (I O)/OI/O = 1 + (I O)/OAnd (I/O) q = q + [(I O)/O] q; q measured quantity ---------- Eq - 1That is a quantity q when measured in real time it would appear as q+ [(I O)/O] q500 years of modern physics and 500,000 of modern physicists is all wrongbecause of this principle (I/O) q = q + [(I O)/O] -------------- Eq - 1

Or quantum = classical + relativisticIf Eq 1 is applied it would expose modern physics as stupidity itself and itwould expose modern astronomy as astrology itself. The thing about thisprinciple given by Eq 1: (I/O) q = q + [(I O)/O] q is that it is flawlessvictory or truth itself

Modern space time physics is all wrong and Arabs real time physicsis flawless is because space timers see detect and measure q as (I/O) q


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and space - timers take the difference [(I O)/O] q as real measurementwhen it is a real time visual effect and nothing real about it; yes, thisquantity [(I O)/O] q is a real time measurement error and modern physicsis based on wrong time measurements. This Phenomenon was discovered in10th century AD by Arab Astronomers and Arab Physicists: What Arab

Physicists said was I: Measurements are made along the line of sight or lineof measurement

This is 950 AD Arabs claim that humans and machines see along the line of sight oalong the line of measurement and that mean any point on the vertical black line wbe measured as the blue line. That is a point location as far as the pink line would measured as the blue line. The angle between the blue line and the pink line is ( which is the light aberrations angle t = arc tan (v/c). The light coming from obje

seen along the line of sight and that meant we do not measure actual distance r0(line)but we measure r0cosine t (blue line) and we escape measuring r0sine which is perpendicular to the line of sight (black line).

In Short, light coming from objects is seen along the line of sight and that meant wcan use real time mathematics to explain what we can see detect and measure and

that would be not r0 but r = r0cosine t + r0cosine t = r0 e (r) t

Or r = real (blue = along line of sight) + imaginary (black = perpendicular toline of sight). Or, r = r0 e (r) t

The absolute value of r = the absolute value ofr0This statement said that light comes along line of sight and that meant we see ligh

projections of objects positions (blue line) and not objects position and this line of or projection of objects position is a constant and it explains Einsteins claims that speed is a constant when light speed projection and not light speed is measured asconstant.

Arabs real time astronomy is actually quantum mechanics r = r0 e (r) t

Light is emitted and not an emitter and humans have no means ofmeasuring light in motion and at best they can take a snap shot.In mathematical languageThen r (, 0) = r 0 e at t = 0

And r (, t) = r 0 e (+ t)= r 0 e e t= r (, 0) e tAnd r (, t) = r (, 0)[cosine t + sine t]And r x (, t) = r x (, 0)cosine tAnd t = cosine-1 [r x (, t) / r x (, 0)]

Then r = r x (, t) - r x (, 0)= r x (, 0)[(cosine t) 1]


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And [r x (, t) - r x (, 0)]/ r x (, 0)= [(1 - 2 sine t/2) 1]= - 2 sine t/2; t = cosine-1 [r x (, t) / r x (, 0)]

rabs real time astronomy:Image = Image = IObject = Object = O- Object = - Object = - O

Image = object + (Image Object)

I = O + (I O)

(I/O) = O/O + [(I O)/O]

(I/O) = 1 + [(I O)/O]Page 8

(I/O) ' 0 = ' 0 + [(I O)/O] ' 0Quantum = classical + relativistic Illusion

I = r; O = r 0Or, (r / r 0) ' 0 = ' 0 + [(r r 0)/ r 0] ' 0And [(r r 0)/ r 0] ' 0Or [- 2sine t/2] ' 0; t = cosine-1 [r x (, t) / r x (, 0)] cosine-1 (r/ r 0)For planet Mercury:

The distance visual effect Error is: [(r m re)/re] mThe quantity: m = (v m/r m) (180/ ) [36526/Tm (days)] (3600) = 70.75With v m = 47.9 km/sec; r m = 58.2 x 106 km; Tm = 88 daysWith r = 58.2 x 109 m = Sun Mercury distanceAnd r e =149.6 x 109 m = Sun Earth distanceWith [(r m re)/re] = [- 2sine t/2] = 0.61[(r m re)/re] m = 0.61 x 70.75 = 43

Planet Distance rX 106km

PlanetOrbit T

Orbitspeed v

inkm/sec

LessEarth

speed

Spinspeed

km/sec

Angular velocity;v/r

arc sec/ century

Mercury 58.2 88 47.9 18.1 .002 70.75Venus 108.2 224.7 35.05 5.7 6.52 10.86Earth 149.6 365.26 29.8 .46511 4.1Mars 227.936 687 24.14 0.2411Jupiter 778.412 4333 13.06 12.6Saturn 1,426.725 10760 9.65 9.87Uranus 2,870.97 30690 6.80 2.59Neptune 4,498 60180 5.43 2.68

Pluto 5906.4 90730 4.74


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Solving Newtons equation in real time ends quantumrelativistic mechanics

Solution: Location r = r r (1) ; Velocity v = r' r (1) + r ' (1)Acceleration = (r" - r') r (1) + (2r'' + r ") (1)

S = m r; State = mass x distanceP = d S/ d t = d (m r)/d t = m (d r/d t) + (d m/d t) rVelocity = v = (d r/d t); mass rate change = m' = (d m/d t)P = m v + m' r; Momentum = change of state = change in location orchange in massF =d P/d t = d S/d t = d [m (d r/d t) + (d m/d t)]/d t

= m d r/d t + (d m/d t) (d r/d t) + (d m/d t) (d r/d t) + (d m/d t) rF = m d r/d t + 2 (d m/d t) (d r/d t) + (d m/d t) r

Force = Change of momentumF = m a + 2 m ' v + m" r

F = - GmM/rOr, Newton's Kepler's equation: F = - GmM/rThen

With d (m r)/dt - (m r) ' = -GmM/r Newton's Gravitational Equation (1)And d (mr')/d t = 0 Kepler's force law (2)

With m = constant, then m can be taken out from both equations (1) and (2)With d r/d t - r ' = - GM/r Newton's Gravitational Equation (1)

And d (r') /d t = 0 Kepler's force law (2)From 2: With m = constant; then d (mr')/d t = 0And m d (r')/d t = 0

And d (r')/d t = 0And r' = hWith (1): d (m r)/dt - (m r) ' = -GmM/rWith m = constantThen m [d r/ d t - r '] = - Gm M/ rAnd [d r/ d t - r '] = - G M/ rLet r =1/uThen d r/d t = -u'/u = - (1/u) (') d u/d = (- '/u) d u/d = - h d u/d And d r /d t = - h 'du/d = - h u [du/d]And - h u [du/d] - (1/u) (hu) = - G MuOr, [du/ d] + u = G M/ h

u = G M/ h + A cosine And r = 1/u = 1/ [G M / h + A cosine ]

= (h/ G M)/ [1 + (Ah/ GM) cosine ]= (h/GM)/ (1 + cosine )

Then r (, 0) = a (1-)/ (1+ cosine )This is Newton's Classical Equation solution of two body problem. Wesolved this equation and we got the motion equation:


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Is: r (, t) = [a (1-)/ (1+ cosine )] which is the equation of anellipse with eccentricity and semi - major axis a, and a semi- minoraxis whose value is b = a [1 - ] and two foci one equals to c = a,and the other foci location equals to - c = - a. Or the motion of oneball around the other ball should be an ellipse with the other ball at

one of the foci +/- a, of the ellipse with semi major axes (- a, a) onx-axis and semi minor axes (-b, b) on y- axis and foci (- c, c) on x-axis again with angle of rotation . If this law to work on two planetsinstead of two balls like planetary motion around the sun, thenAstronomers should see this motion of a planet moving around the sunin an ellipse with the sun at one of its foci.

What astronomers saw was not an ellipse but a rotating ellipse like theellipse below wth rotating angle

M

m


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When the areas size A are sliced equally it was found that the times spent byplanets orbiting around the Sun and making areas A each are equal also.Or, r (0) ' (0) = r (1) ' (1) = r (2) ' (2) = r (3) ' (3) = --

= location x [angular speed] = constant= Areal velocity

If r '= h

Then differentiating with respect to timeThen d (r ')/ d t= d h/ d tAnd 2 r r + r = 0Or 2 (r /r) = - (/) = +

The r = r0 e( + ) t

And = 0 e 2 ( + ) t

With r = r0 e t; = 0In real time r = (, 0) = a (1-)/ (1+ cosine ) e t

With r (0) ' (0) = r (1) ' (1)Then ' (1) = [r (0)/ r (1)]' (0)

And ' (1) = {[e 2 t] ' (0)And (1) = {[cosine 2 t + sine 2 t] 1}' (0) (1) = (x) + (y)

= [cosine 2 t + sine 2 t] ' (0) (x) = [cosine 2 t] ' (0) (x) = [1 2 sine t] ' (0)

M

m


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(x) - ' (0) = - 2' (0) sine t W = (x) - ' (0) = - 2' (0) sine t

= -2(2) [ (1-)]/T (1-) ] sine tAnd ' (0) = h/r (0) = 2 a b/T a = 2 (1-)]/T (1-)

W = - 4 ) [ (1-)]/T (1-) ] sine tIf this apsidal motion is to be found as visual effects, thenWith, v = spin velocity; v* = orbital velocityAnd v/c = (v* + v)/c = tan t W = -4 [ (1-)]/T (1-) ] sine {Inverse tan [(v* + v)/c]}radiansMultiplication by 180/ to change to degrees W = (-720/T) {[ (1-)]/ (1-) } sine {Inverse tan [(v* + v)/c]}DegreesAnd multiplication by 1 century = 36526 days and using T in daysW (ob) = (-720x36526/Tdays) {[ (1-)]/ (1-) } x

sine {Inverse tan [(v* + v)/c]} degrees/100 years

Astronomy re - written

W (calculated) = (-720x36526/T) {[ (1- )]/ (1- ) ]} [(v + v*)/degrees/100 years

Primary

Secondary

v(p) v* (p) v (p) v* (p) v (p) v* (p) v (p) V* (p)

v(s) v* (s) Spin=[,]

[,]=orbit

[,][,] [,][,] [,][,]

Spin results v(p) + v(s) v(p) + v(s) - v(p) + v(s) -v(p) + v(s)

Orbit results v*(p) + v*(s) -v*(p) + v*(s) v* (p) + v*(s) -v* (p) + v* (s)

Examples AS CAMv (s) v* (s) [,][,] [,][,] [,][,] [,][,]

Spin results v(p) + v(s) v(p) + v(s) -v(p) + v(s) -v(p) + v(s)

Orbit results v*(p) - v*(s) -v*(p) - v*(s) v*(p) - v*(s) -v* (p) - v* (s)

Examples

v (p) v*(s) [,][,] [,][,] [,][,] [,][,]

Spin results v(p) - v(s) v(p) - v(s) -v(p) - v(s) -v(p) - v(s)

Orbit results v*(p) + v*(s) -v*(p) + v*(s) v*(p) + v*(s) -v* (p) + v* (s)

Examples AS CAM

v (s) V*(s) [,][,] [,][,] [,][,] [,][,]

Spin results v(p) - v(s) v(p) - v(s) -v(p) - v(s) -v(p) - v(s)Orbit results v*(p) - v*(s) -v*(p) - v*(s) v*(p) - v*(s) -v* (p) - v* (s)

Examples AS CAM


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1- Planet Mercury axial "apparent" rotation rate W = (-720x36526x3600/T) {[ (1-]/ (1-) } (v* + v/c) seconds of arc per century

The circumference of an ellipse: 2a (1 - /4 + 3/16()- --.) 2a (1-/4); R =a (1-/4)

Where v* (p) = [G M / (m + M) a (1-/4)] [GM/a (1-/4)];m


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Planet orbital velocity or primary velocity:And v* (m) = v (m) = [GM/ (m + M) a (1-/4)]R =a (1-/4)Calculations: (1- /4) = 0.9928[ (1-)]/ (1-) = 1.43

With a = [R (m)/r (m)]= (2.57/0.1499) (0.696x109) = 11.9327x109And v* (m) = [GM/ (m + M) a (1- /4)] = 110km/sec= [6.673x10-11 (2.5) (2 x 1030)/ (5.8) 11.932x109 (0.9928)]= 110.178km/secAnd v* (M) = [GM/ (m + M) a (1- /4)]= [6.673x10-11 (3.3) (2 x 1030)/ (5.8) 11.932x109 (0.9928)]= 145.435 km/secSpin: v = 40 + 30=70km/secAnd v* (e) = v* Earth = 29.8 km/secAnd v (e) = 0.465 km/sec

Then v* + v = v* (m) + v* (M) + v* (e) + v (m) + v (M) + v (e)= 110.178 + 145.435 + 70 + 29.8 0.465 = 355 m/sec[ (1-)]/ (1-) = 1.43; T = 3.431days

W= (-720x36526/T) x { [(1-)] (1-) } {[v* + v]/c}

W= (-720x36526/3.431) x (1.43) (355/ 300,000) = 15/century

Dr Guinan and DR Maloney 1989: W= 15/century 1989

Einstein and 500 years of modern physics: 44.3/ century

Another way to solve this problem: m = (v m/r m) (180/ ) [36526/Tm (days)] (3600) = 70.75 Mercury

For planet Mercury 70.75 (29.8 0.465)/47.9 = 43For As Camelopardalis: m = (v m/r m) (180/ ) [36526/Tm (days)] (3600)= 12.928[(145 + 30)/ (110 + 30)] (12.928) = 15Conclusion is:All rights reservedThe motion of a particle in space is given by a time independent particlemotion ofr = r 0 e ; Ground state

How you see this particle is a time dependent wave motionOf: r = r 0 e (+ t); excited state!

The difference between a particle time dependent motion and timeindependent motion is relativistic IllusionsWhen applied to planets and stars motion it is a flawless victory!

Keplers law in real time 600 years before KeplerAcceleration is distance /t and if we fix time t = T and distance r = a


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Then acceleration = a/T; If we take T = t and r = a then acceleration =constant and acceleration = k/r 0r acceleration = k/aThat is we can make a time dependent acceleration r/t a time independentacceleration a /T and establish a constant time that is replaceable by aconstant space dimension k/a and: a/T = k/a

Or Keplers law:Of: a/T = k = constant and If we use Arabs real time idea of (r r0)/r0Or, a1/ T1 = a2/ T2Or, a1/ a2 = (T1/ T2)2/3

And (a1 - a2)/ a2 = (T1/ T2)2/3 1Or (am a e)/ a e = (Tm/ Te) 2/3 1; space time equivalence

= [(Tm/ Te) 2/3 1] (47.9/58.2 x 106) [(180/) (3600) (26526/88)] = [(88/ 365.26) 2/3 1] (47.9/58.2 x 106) [(180/) (3600) (26526/88)]= 43 arc sec /century

The solution is a particle you dummy and the factyou see a wave you do not have to be an idiot likeyour Harvard MIT or Cal Tech Nobel Physicist!

wave - particle duality solution

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