satellite geodesy: kepler orbits, kaula ch. 2+3.i1.2a

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U N ICA EU Research ContractsSeminar, Brussels, 29-30 M ay 2000.05.23 Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a Basic equation: Acceleration Connects potential, V, and geometry. (We disregard disturbing forces – friction). C.C.Tscherning, 2007-10-25. i i i i X V dt t X d t X t X 2 2 ) ( ) ( tim of function a as s coordinate - orbit ) (

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Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a. Basic equation: Acceleration Connects potential, V, and geometry. (We disregard disturbing forces – friction). C.C.Tscherning, 2007-10-25. Velocity: Integration along orbit. Position: one integration more. C.C.Tscherning, 2007-10-25. - PowerPoint PPT Presentation

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Page 1: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

• Basic equation: Acceleration

• Connects potential, V, and geometry. (We disregard disturbing forces – friction).

C.C.Tscherning, 2007-10-25.

i

ii

i

X

V

dt

tXdtX

tX

2

2 )()(

timeoffunction a as scoordinate-orbit)(

Page 2: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Velocity: Integration along orbit.

• Position: one integration more

C.C.Tscherning, 2007-10-25.

)()()(

)( 02

2

1

1

0

1tXdt

dt

tXd

dt

tdXtX i

t

t

it

ii

Page 3: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

• We must know (approximatively) the orbit to make the integration.

• The equation connects the position and velocity with parameters expressing V.

• Parameters: kMCij

Orbit integration and parameter determination

C.C.Tscherning, 2007-10-25.

Page 4: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

• Directions and distances from Earth using Cameras, lasers, radar-tracking, time-differences

• Distances from satellites to ”point” on Earth surface (also ”cross-overs”)

• Range rates: Doppler effect, contineous tracking.

• Measurements in or between satellites: gradiometry, GPS-positions, ranging

Observations

C.C.Tscherning, 2007-10-25.

Page 5: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

• Spherical harmonic coefficients, kMCij

• Positions of ground tracking stations

• Changes to Earth Rotation and pole-position

• Tides (both oceanic and solid earth)

• Drag-coefficients, air-density

• Contributions from Sun and Moon.

Parameters

C.C.Tscherning, 2007-10-25.

Page 6: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Ordinary differential equations

• Change from 3 second order equations to 6 first-order equations:

C.C.Tscherning, 2007-10-25.

i

i

i

i

i

X

V

dt

dXdt

X

X

V

dt

X

dY:1'.order of 6

d :order 2'. of 3

i

2

2

Page 7: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Coordinate transformation in 6D-space

• New coordinates qi and pi .

C.C.Tscherning, 2007-10-25.

),,,,,(

),,,,,(

321321

321321

pppqqqV

XXXXXXV

q

V

dt

dp

p

V

dt

dq

i

i

i

ii

Page 8: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

(q,p) selected so orbits straight lines

• If

• Possible also so that kmCij ”amplified”.

C.C.Tscherning, 2007-10-25.

0 ,0

p)(q, find topossible ,

dt

dp

dt

dqr

kMV

ii

Page 9: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Kepler orbit

• If potential V=km/r:• Orbit in plane through origin (0).• Is an ellipse with one focus in origin

C.C.Tscherning, 2007-10-25.

Page 10: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Geometry

• E and f

C.C.Tscherning, 2007-10-25.

Page 11: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Kepler elements

• i=inclination, Ω=longitude of ascending node (DK: knude)

• e=excentricity, a=semi-major axis,

• ω=argument of perigaeum, f+ ω=”latitude”.

• M=E-esinE=Mean anomaly (linear in time !)

C.C.Tscherning, 2007-10-25.

Page 12: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

From CIS to CTS

• We must transform from Conventional Inertial System to Conventional Terrestrial System using siderial time, θ:

• Rotation Matrix

C.C.Tscherning, 2007-10-25.

3

2

1

3

100

0cossin

0sincos

)(

u

u

u

uR

Page 13: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

From q-system to CIS

• 3 rotations. Ri with integer i subscript is rotation about i-axis. Rxu is rotation from u to x.

xuqxquqx RRRRiRRR ),()()( 313

C.C.Tscherning, 2007-10-25.

Page 14: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Elliptic orbit

• We use spherical coordinates r,λ in (q1,q2)-plane

vector-unit is // 3 rxrxkx

C.C.Tscherning, 2007-10-25.

Page 15: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Angular momentum

• λ is arbitrary := 0 !

C.C.Tscherning, 2007-10-25.

xyyxx

xyyx

xy

xy

hr

rr

rrr

h and /1

1

so ),/(tan

! conserved momentumangular

:r with gmultiplyin ,02

/)(

222

1

2

22

Page 16: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Integration

• With u=1/r

C.C.Tscherning, 2007-10-25.

Page 17: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Integration

C.C.Tscherning, 2007-10-25.

20

22

2

2422

222

2

/)cos(1

/

/1

so ,)r(-rin result theUse

hAur

hud

ud

ruhud

uduh

Page 18: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Ellipse as solution

• If ellipse with center in (0,0)

C.C.Tscherning, 2007-10-25.

)1(

)cos(

)1(

1

r

1or

))cos(1(

e-a(1r

degree-2. of polynomiumith equation w

),1( with),sin(

)cos(

r)(f, scoordinate spherical use weand ,1

22

2)

222

2

2

2

2

ea

fe

eafe

eabfr

feaeba

Page 19: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Expressed in orbital plane

C.C.Tscherning, 2007-10-25.

)cos1(

,sin1

)(cos

:E anomaly, excentric using expresed

)1(,)1(

,

22

21

22

1

220

Eeaqqr

Eeaq

eEaaeq

eahea

eAf

Page 20: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Parameter change

C.C.Tscherning, 2007-10-25.

)derivation long a(after 1/

)2/()cos12)sin(2(

then ,)1(

sin)1(

)/1(

:E with f substitute weand , then

22

221

22

212

2

2

22

2

eeq

rEeaqEaqdE

dr

qqrdfea

qerdr

fea

er

df

rdr

df

dr

hfrf

Page 21: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Further substitution

C.C.Tscherning, 2007-10-25.

2/32/1

0

2

222

222

and perigaeum of passagefor me with t ti

),()cos1(

)1(

)1

)1()cos1(

an

ttnMEe

ea

dt

dEq

e

e

qer

eaEea

Page 22: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Transformation to CIS

C.C.Tscherning, 2007-10-25.

Page 23: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Velocity

C.C.Tscherning, 2007-10-25.

ar

vVT

22

2

Page 24: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

From orbital plane to CIS

• .

C.C.Tscherning, 2007-10-25.

f. findcan weifknown )/(tan

then,)()(

put we),/)((tan

))/((tan

)0,,( toorthogonal ),,(

121

21

32/12

22

11

211

21321

ppf

xRiRp

hhhi

hh

qqhhhh

Page 25: Satellite geodesy: Kepler orbits, Kaula Ch. 2+3.I1.2a

UNICA EU Research Contracts Seminar, Brussels, 29-30 May 2000.05.23

Determination of f

• .

C.C.Tscherning, 2007-10-25.

))/(cossin1(tan)/(tan

))(/(sin

) (from )/()(cos

))/(1(),2/(

)/(

2112

1

2/1

22

21

2/122

2/1222

eEEeqqf

aerrE

qqraeraE

ahervra

rhvr