Presentation is loading. Please wait.

Presentation is loading. Please wait.

New Trends in Astrodynamics and Applications Princeton, NJ. June 3-4 2005 Hamilton-Jacobi Modelling of Relative Motion for Formation Flying 1/16 by Egemen.

Similar presentations


Presentation on theme: "New Trends in Astrodynamics and Applications Princeton, NJ. June 3-4 2005 Hamilton-Jacobi Modelling of Relative Motion for Formation Flying 1/16 by Egemen."— Presentation transcript:

1 New Trends in Astrodynamics and Applications Princeton, NJ. June Hamilton-Jacobi Modelling of Relative Motion for Formation Flying 1/16 by Egemen Kolemen 1, N. Jeremy Kasdin 1 & Pini Gurfil 2 1.Princeton University, Mechanical & Aerospace Engineering 2.Technion Israel Institute of Technology, Aerospace Engineering

2 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 2/28 Content 2. Hamilton Jacobi Analysis 3. Results - Eccentric Orbit 5. Conclusions 4. Results - J 2, J 3, J 4 Perturbation 1. Literature

3 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 3/28 Formation Flying Co-observing Stereo Imaging Interferometry Large Constellations In situ observations Aerobots Tethered Interferometry Space Station “Aircraft Carrier” to Fleets of Distributed Spacecraft Sensor Webs Multi-point observing

4 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 4/28 Dynamical Modeling of Relative Motion Control is expensive Use natural forces to control Aim: 1.Initial conditions Bounded orbits 2.Relative Trajectory Position, velocity 3.Local measurement / Local Control suitability Artist’s impressions of Orion/Emerald Spacecrafts

5 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 5/28 Background Linearized relative motion in a Cartesian rotating frame. (C-W, `60) Described linear relative motion using orbital elements (Schaub, Vadali, Alfriend, `00) Applied symmetry and reduction technique to J 2 perturbation (Koon, Marsden, Murray `01) Used approximate generating function for the relative Hamiltonian (Guibout, Scheeres, `04) Provided detailed description of our method and J 2 solution (Kasdin, Gurfil, & Kolemen, `05)

6 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 6/28 Aim: To solve the rendezvous problem Two-body equation: where r is the position of the satellite, where  is the relative position, Linearizing the equation around  =0 and keeping only the 1 st order terms, we get: Clohessy-Wiltshire (C-W) Equations Relative motion in rotating Euler-Hill reference frame

7 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 7/28 Clohessy-Wiltshire (C-W) Equations Periodic motion in z-direction. A stationary mode, an oscillatory mode, and a drifting mode in the x-y plane. The non-drifting condition: 2 by 1 ellipse x-y plane.

8 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 8/28 How to extend this solution? What is the effect of perturbations on periodic orbits? How do we get into these periodic orbits? Not only finding Initial Conditions but finding Periodic Orbits. Approach: –Solve Hamilton-Jacobi Equations. –Express the periodic relative orbits by canonical elements. –Perform perturbation analysis on these elements.

9 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 9/28 Canonical Analysis of Relative Motion Velocity in the rotating frame: Kinetic Energy: Potential Energy: Relative motion in rotating frame

10 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 10/28 The Hamiltonian Separate low and higher order Hamiltonian: The unperturbed Hamiltonian: Corresponds to C-W equations: Solve Hamilton-Jacobi Equations for the 6 constants of motion.

11 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 11/28 Hamilton-Jacobi (H-J) Solution Transform Cartesian elements to new constants using H-J Theory. Termed Epicyclic Elements The new Hamiltonian: Cartesian coordinates:

12 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 12/28 Physical meaning of the Epicyclic Elements Osculating 2:1 elliptic relative orbit –  1  size –  3  drift in y-axis –Q 3  center position in y-axis –Q 1  phase Osculating elliptic relative orbit

13 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 13/28 Modified Epicyclic Elements For ease of calculations, symplectic transformation to amplitude only variable: The new Hamiltonian: Cartesian coordinates:

14 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 14/28 Perturbations to Relative Motion Perturbation Analysis: Perturbing Hamiltonian: Hamilton’s Equations: Transform the perturbation on the relative orbit to perturbations on the canonical elements.

15 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 15/28 Relative Motion Around Eccentric Orbits Relative velocity: Find Hamiltonian, expand in eccentricity: 1 st order perturbing Hamiltonian: Relative motion around an eccentric orbit

16 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 16/28 Relative Motion Around Eccentric Orbits Variation of epicyclic elements: Solution: No drift condition for 1 st order:

17 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 17/28 Eccentricity/Nonlinearity Perturbation Results e =  m/orbit e = mm/orbit e = cm/orbit Third order no drift condition. Approximation good up to e ~ 0.03 Code: ~ekolemen/eccentricity.m

18 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 18/28 Placing Multiple Satellites on Relative Orbit Specify: Size in x-y plane and z-plane. Phase of each satellite Place a group of satellites in one relative orbit.

19 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 19/28 Earth Oblateness Perturbation Earth’s Oblateness ( J 2 zonal harmonic) is often the largest perturbation. Axially symmetric gravitational potential zonal harmonics: where  is the spacecraft’s latitude angle: Z is the distance from the Equatorial Plane and the J k 's:

20 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 20/28 Effect of the J 2 Perturbation on a single spacecraft The long term variation of the mean orbital elements: where a, e, i, , u orbital element and n mean motion. And, Note: For circular orbits, argument of perigee,  does not make sense. Regression of the ascending node under the J 2 perturbation

21 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 21/28 The Average J 2 Drifting Frame Rotating with the average J 2 drift: The velocity of the follower: First order no drift condition Angular velocity of the average J 2 drifting frame

22 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 22/28 Periodic Orbits around J 2 and J 2 2 drifting frame 3 different types of periodic orbits. Comparison with differential orbital elements    Invariance under    i,  e,  a: Solutions for   u: Invariance under u.   i,  e,  a uu

23 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 23/28 Families of Periodic Orbit around L 2 NORTHERN HALO Orbit LISSAJOUS Orbits NORTHERN QUASIHALO Orbits VERTICAL LYAPUNOV Orbit SOUTHER Orbits HORIZONTAL LYAPUNOV Orbit (?) Univ. Barcelona: Jorba, Gomez, Simo Univ. Catalunya: Masdemont (?)

24 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 24/28 Reference Frames and Relative Motion Bounded Orbit 2 Bounded Orbit 1 Mean Rotating Frame Osculating Rotating Frame Real Relative Motion

25 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 25/28 J 2 and J 2 2 Periodic Solutions (Two Spacecrafts) Short Term: 20 OrbitsLong Term: 200 Orbits Error: 30cm/orbit

26 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 26/28 Tumbling Effect Tumbling of the Relative Orbit Examples : Figure: S. A. Schweighart, “Development and Analysis of a High Fidelity Linearized J2 Model for Satellite Formation Flying”

27 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 27/28 5 boundedness conditions, Constraining all the parameters except the  u offset.  One osculating orbit for one mean orbit. Higher Order Zonal Perturbation: J 2, J 2 2, J 3, J 4 Relative motion around the rotating frameRelative motion around osculating orbit Error: 30cm/orbit

28 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 28/28 Conclusion A Hamiltonian approach to solve for the relative motion is applied. Bounded relative motion for nonlinearity and eccentricity perturbation is solved. Effect of zonal harmonics, J 2, J 3, and J 4 on the relative bounded orbit is investigated. Outlook: Combine eccentricity and zonal harmonics perturbations. Relative Motion for J 2, J 3, J 4 perturbations

29 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 29/28 References Koon, Lo, Marsden and Ross, “Dynamical Systems, the Three-Body Problem and Space Mission Design”, To be published Jorba, Masdemont, “Dynamics in the center manifold of the collinear points of the restricted three body problem”, Physica D 132 (1999) 189–213 Jorba, “A Methodology for the Numerical Computation of Normal Forms, Centre Manifolds and First Integrals of Hamiltonian Systems”, Experimental Mathematics 8, Gomez, Masdemont, Simo, “Quasi-Periodic Orbits Associated with the Libration Points”, JAS, 1998(2), 46, S. A. Schweighart, “Development and Analysis of a High Fidelity Linearized J2 Model for Satellite Formation Flying” Master of Science, MIT, June 2001 T. A. Lovella, S. G. Tragesser, “Near-Optimal Reconfiguration and Maintenance of Close Spacecraft Formations” Ann. N.Y. Acad. Sci. 1017: 158–176 (2004).

30 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 30/28 Clohessy, W.H. & R.S. Wiltshire Terminal guidance system for satellite rendezvous. J. Astronaut. Sci. 27(9): Carter, T.E. & M. Humi Fuel-optimal rendezvous near a point in general Keplerian orbit. J. Guid. Control Dynam. 10(6): Inalhan, G., M. Tillerson & J.P. How Relative dynamics and control of spacecraft formations in eccentric orbits. J. Guid. Control Dynam. 25(1): Gim, D.W. & K.T. Alfriend The state transition matrix of relative motion for the perturbed non-circular reference orbit. Proceedings of the AAS/AIAA Space Flight Mechanics Meeting, Santa Barbara, CA, February. AAS Alfriend, K.T. & H. Schaub Dynamics and control of spacecraft formations: challenges and some solutions. J. Astronaut. Sci. 48(2): Hill, G.W Researches in the lunar theory. Am. J. Math. 1: Schaub, H., S.R. Vadali & K.T. Alfriend Spacecraft formation flying control using mean orbital elements. J. Astronaut. Sci. 48(1): Namouni, F Secular interactions of coorbiting objects. Icarus 137: Gurfil, P. & N.J. Kasdin Nonlinear modeling and control of spacecraft relative motion in the configuration space. Proceedings of the AAS/AIAA Spacecflight Mechanics Meeting, Puerto Rico, February. Karlgaard, C.D. & F.H. Lutze Second-order relative motion equations. Proceedings of the AAS/AIAA Astrodynamics Conference, Quebec City, Quebec, July. AAS Alfriend, K.T., H. Yan & S.R. Vadali Nonlinear considerations in satellite formation flying. Proceedings of the 2002 AIAA/AAS Astrodynamics Specialist Conference, Monterey, CA, August. AIAA Koon, W.S., J.E. Marsden & R.M. Murray J2 dynamics and formation flight. Proceedings of the 2001 AIAA Guidance, Navigation, and Control Conference, Montreal, Canada, August. AIAA Broucke, R.A Motion near the unit circle in the three-body problem. Celest. Mech. Dynam. Astron. 73(1): Goldstein, H Classical Mechanics. Addison-Wesley. Battin, R.H An Introduction to the Mathematics and Methods of Astrodynamics. AIAA.

31 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 31/28 Clohessy, W.H. & R.S. Wiltshire Terminal guidance system for satellite rendezvous. J. Astronaut. Sci. 27(9): Carter, T.E. & M. Humi Fuel-optimal rendezvous near a point in general Keplerian orbit. J. Guid. Control Dynam. 10(6): Inalhan, G., M. Tillerson & J.P. How Relative dynamics and control of spacecraft formations in eccentric orbits. J. Guid. Control Dynam. 25(1): Gim, D.W. & K.T. Alfriend The state transition matrix of relative motion for the perturbed non-circular reference orbit. Proceedings of the AAS/AIAA Space Flight Mechanics Meeting, Santa Barbara, CA, February. AAS Alfriend, K.T. & H. Schaub Dynamics and control of spacecraft formations: challenges and some solutions. J. Astronaut. Sci. 48(2): Hill, G.W Researches in the lunar theory. Am. J. Math. 1: Schaub, H., S.R. Vadali & K.T. Alfriend Spacecraft formation flying control using mean orbital elements. J. Astronaut. Sci. 48(1): Namouni, F Secular interactions of coorbiting objects. Icarus 137: [CrossRef][CrossRef] Gurfil, P. & N.J. Kasdin Nonlinear modeling and control of spacecraft relative motion in the configuration space. Proceedings of the AAS/AIAA Spacecflight Mechanics Meeting, Puerto Rico, February. Karlgaard, C.D. & F.H. Lutze Second-order relative motion equations. Proceedings of the AAS/AIAA Astrodynamics Conference, Quebec City, Quebec, July. AAS Alfriend, K.T., H. Yan & S.R. Vadali Nonlinear considerations in satellite formation flying. Proceedings of the 2002 AIAA/AAS Astrodynamics Specialist Conference, Monterey, CA, August. AIAA Koon, W.S., J.E. Marsden & R.M. Murray J2 dynamics and formation flight. Proceedings of the 2001 AIAA Guidance, Navigation, and Control Conference, Montreal, Canada, August. AIAA Broucke, R.A Motion near the unit circle in the three-body problem. Celest. Mech. Dynam. Astron. 73(1): [CrossRef][CrossRef] Goldstein, H Classical Mechanics. Addison-Wesley. Battin, R.H An Introduction to the Mathematics and Methods of Astrodynamics. AIAA.

32 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 32/28 Clohessy-Wiltshire Equations

33 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 33/28 Background W.H. Clohessy, R. S. Wiltshire, “Terminal Guidance for Satellite Rendezvous”, 1960 TAMU H. Schaub, S. R. Vadali, K. T. Alfriend, “Spacecraft Formation Flying Control Using Mean Orbital Elements”, 2000 MIT G. Inalhan, M. Tillerson, J. P. How, “Relative Dynamics and Control of Spacecraft Formation in Eccentric Orbits”, 2002 Princeton/Technion –N. J. Kasdin and P. Gurfil, “ Canonical Modelling of Relative Spacecraft Motion via Epicyclic Orbital Elements ”, In publish Caltech W. S. Koon, J. E. Marsden and R. M. Murray, “J2 DYNAMICS AND FORMATION FLIGHT”, AIAA UMich V.M. Guibout, D.J. Scheeres, “Solving relative two-point boundary value problems: Application to spacecraft formation flight transfer” Journal of Guidance, Control, and Dynamics 27(4): Univ. Surrey Y. Hashida, P. Palmer, “Epicyclic Motion of Satellites Under Rotating Potential”, Journal of Guidance, Control and Dynamics, Vol. 25, No. 3, pp , 2002.

34 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 34/28 Perturbations Question: H^{(1)}, perturbing Hamiltonian, How do we get into these periodic orbits? How will be the form of the new periodic orbits? Answer: Hamilton’s

35 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 35/28 Analytical Solution for the Base Orbit Kozai  Sgp Brower  Sgp4 Hoots  HANDE  Von Ziepel 1 st order in J 2 short term (not precise) Coffey and Deprit Vinti  Lie Method Too many terms

36 “Hamilton-Jacobi Modelling of Relative Motion for Formation Flying” E. Kolemen, J. Kasdin, P. Gurfil 36/28


Download ppt "New Trends in Astrodynamics and Applications Princeton, NJ. June 3-4 2005 Hamilton-Jacobi Modelling of Relative Motion for Formation Flying 1/16 by Egemen."

Similar presentations


Ads by Google