On the Location of the Ring Around the Dwarf Planet Haumea
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Astrodynamics
Politecnico di Torino SEEDS SpacE Exploration and Development Systems Astrodynamics II Edition 2006 - 07 - Ver. 2.0.1 Author: Guido Colasurdo Dipartimento di Energetica Teacher: Giulio Avanzini Dipartimento di Ingegneria Aeronautica e Spaziale e-mail: [email protected] Contents 1 Two–Body Orbital Mechanics 1 1.1 BirthofAstrodynamics: Kepler’sLaws. ......... 1 1.2 Newton’sLawsofMotion ............................ ... 2 1.3 Newton’s Law of Universal Gravitation . ......... 3 1.4 The n–BodyProblem ................................. 4 1.5 Equation of Motion in the Two-Body Problem . ....... 5 1.6 PotentialEnergy ................................. ... 6 1.7 ConstantsoftheMotion . .. .. .. .. .. .. .. .. .... 7 1.8 TrajectoryEquation .............................. .... 8 1.9 ConicSections ................................... 8 1.10 Relating Energy and Semi-major Axis . ........ 9 2 Two-Dimensional Analysis of Motion 11 2.1 ReferenceFrames................................. 11 2.2 Velocity and acceleration components . ......... 12 2.3 First-Order Scalar Equations of Motion . ......... 12 2.4 PerifocalReferenceFrame . ...... 13 2.5 FlightPathAngle ................................. 14 2.6 EllipticalOrbits................................ ..... 15 2.6.1 Geometry of an Elliptical Orbit . ..... 15 2.6.2 Period of an Elliptical Orbit . ..... 16 2.7 Time–of–Flight on the Elliptical Orbit . .......... 16 2.8 Extensiontohyperbolaandparabola. ........ 18 2.9 Circular and Escape Velocity, Hyperbolic Excess Speed . .............. 18 2.10 CosmicVelocities -
Flight and Orbital Mechanics
Flight and Orbital Mechanics Lecture slides Challenge the future 1 Flight and Orbital Mechanics AE2-104, lecture hours 21-24: Interplanetary flight Ron Noomen October 25, 2012 AE2104 Flight and Orbital Mechanics 1 | Example: Galileo VEEGA trajectory Questions: • what is the purpose of this mission? • what propulsion technique(s) are used? • why this Venus- Earth-Earth sequence? • …. [NASA, 2010] AE2104 Flight and Orbital Mechanics 2 | Overview • Solar System • Hohmann transfer orbits • Synodic period • Launch, arrival dates • Fast transfer orbits • Round trip travel times • Gravity Assists AE2104 Flight and Orbital Mechanics 3 | Learning goals The student should be able to: • describe and explain the concept of an interplanetary transfer, including that of patched conics; • compute the main parameters of a Hohmann transfer between arbitrary planets (including the required ΔV); • compute the main parameters of a fast transfer between arbitrary planets (including the required ΔV); • derive the equation for the synodic period of an arbitrary pair of planets, and compute its numerical value; • derive the equations for launch and arrival epochs, for a Hohmann transfer between arbitrary planets; • derive the equations for the length of the main mission phases of a round trip mission, using Hohmann transfers; and • describe the mechanics of a Gravity Assist, and compute the changes in velocity and energy. Lecture material: • these slides (incl. footnotes) AE2104 Flight and Orbital Mechanics 4 | Introduction The Solar System (not to scale): [Aerospace -
Solar System Planet and Dwarf Planet Fact Sheet
Solar System Planet and Dwarf Planet Fact Sheet The planets and dwarf planets are listed in their order from the Sun. Mercury The smallest planet in the Solar System. The closest planet to the Sun. Revolves the fastest around the Sun. It is 1,000 degrees Fahrenheit hotter on its daytime side than on its night time side. Venus The hottest planet. Average temperature: 864 F. Hotter than your oven at home. It is covered in clouds of sulfuric acid. It rains sulfuric acid on Venus which comes down as virga and does not reach the surface of the planet. Its atmosphere is mostly carbon dioxide (CO2). It has thousands of volcanoes. Most are dormant. But some might be active. Scientists are not sure. It rotates around its axis slower than it revolves around the Sun. That means that its day is longer than its year! This rotation is the slowest in the Solar System. Earth Lots of water! Mountains! Active volcanoes! Hurricanes! Earthquakes! Life! Us! Mars It is sometimes called the "red planet" because it is covered in iron oxide -- a substance that is the same as rust on our planet. It has the highest volcano -- Olympus Mons -- in the Solar System. It is not an active volcano. It has a canyon -- Valles Marineris -- that is as wide as the United States. It once had rivers, lakes and oceans of water. Scientists are trying to find out what happened to all this water and if there ever was (or still is!) life on Mars. It sometimes has dust storms that cover the entire planet. -
The Trans-Neptunian Haumea
Astronomy & Astrophysics manuscript no. main c ESO 2018 October 22, 2018 High-contrast observations of 136108 Haumea? A crystalline water-ice multiple system C. Dumas1, B. Carry2;3, D. Hestroffer4, and F. Merlin2;5 1 European Southern Observatory. Alonso de Cordova´ 3107, Vitacura, Casilla 19001, Santiago de Chile, Chile e-mail: [email protected] 2 LESIA, Observatoire de Paris, CNRS. 5 place Jules Janssen, 92195 Meudon CEDEX, France e-mail: [email protected] 3 European Space Astronomy Centre, ESA. P.O. Box 78, 28691 Villanueva de la Canada,˜ Madrid, Spain 4 IMCCE, Observatoire de Paris, CNRS. 77, Av. Denfert-Rochereau, 75014 Paris, France e-mail: [email protected] 5 Universit Paris 7 Denis Diderot. 4 rue Elsa Morante, 75013 Paris, France e-mail: [email protected] Received 2010 May 18 / Accepted 2011 January 6 ABSTRACT Context. The trans-neptunian region of the Solar System is populated by a large variety of icy bodies showing great diversity in orbital behavior, size, surface color and composition. One can also note the presence of dynamical families and binary systems. One surprising feature detected in the spectra of some of the largest Trans-Neptunians is the presence of crystalline water-ice. This is the case for the large TNO (136 108) Haumea (2003 EL61). Aims. We seek to constrain the state of the water ice of Haumea and its satellites, and investigate possible energy sources to maintain the water ice in its crystalline form. Methods. Spectro-imaging observations in the near infrared have been performed with the integral field spectrograph SINFONI mounted on UT4 at the ESO Very Large Telescope. -
New Closed-Form Solutions for Optimal Impulsive Control of Spacecraft Relative Motion
New Closed-Form Solutions for Optimal Impulsive Control of Spacecraft Relative Motion Michelle Chernick∗ and Simone D'Amicoy Aeronautics and Astronautics, Stanford University, Stanford, California, 94305, USA This paper addresses the fuel-optimal guidance and control of the relative motion for formation-flying and rendezvous using impulsive maneuvers. To meet the requirements of future multi-satellite missions, closed-form solutions of the inverse relative dynamics are sought in arbitrary orbits. Time constraints dictated by mission operations and relevant perturbations acting on the formation are taken into account by splitting the optimal recon- figuration in a guidance (long-term) and control (short-term) layer. Both problems are cast in relative orbit element space which allows the simple inclusion of secular and long-periodic perturbations through a state transition matrix and the translation of the fuel-optimal optimization into a minimum-length path-planning problem. Due to the proper choice of state variables, both guidance and control problems can be solved (semi-)analytically leading to optimal, predictable maneuvering schemes for simple on-board implementation. Besides generalizing previous work, this paper finds four new in-plane and out-of-plane (semi-)analytical solutions to the optimal control problem in the cases of unperturbed ec- centric and perturbed near-circular orbits. A general delta-v lower bound is formulated which provides insight into the optimality of the control solutions, and a strong analogy between elliptic Hohmann transfers and formation-flying control is established. Finally, the functionality, performance, and benefits of the new impulsive maneuvering schemes are rigorously assessed through numerical integration of the equations of motion and a systematic comparison with primer vector optimal control. -
Taxonomy of Trans-Neptunian Objects and Centaurs As Seen from Spectroscopy? F
A&A 604, A86 (2017) Astronomy DOI: 10.1051/0004-6361/201730933 & c ESO 2017 Astrophysics Taxonomy of trans-Neptunian objects and Centaurs as seen from spectroscopy? F. Merlin1, T. Hromakina2, D. Perna1, M. J. Hong1, and A. Alvarez-Candal3 1 LESIA – Observatoire de Paris, PSL Research University, CNRS, Sorbonne Universités, UPMC Univ. Paris 06, Univ. Paris Diderot, Sorbonne Paris Cité, 5 place Jules Janssen, 92195 Meudon, France e-mail: [email protected] 2 Institute of Astronomy, Kharkiv V. N. Karin National University, Sumska Str. 35, 61022 Kharkiv, Ukraine 3 Observatorio Nacional, R. Gal. Jose Cristino 77, 20921-400 Rio de Janeiro, Brazil Received 4 April 2017 / Accepted 19 May 2017 ABSTRACT Context. Taxonomy of trans-Neptunian objects (TNOs) and Centaurs has been made in previous works using broadband filters in the visible and near infrared ranges. This initial investigation led to the establishment of four groups with the aim to provide the mean colors of the different classes with possible links with any physical or chemical properties. However, this taxonomy was only made with the Johnson-Cousins filter system and the ESO J, H, Ks filters combination, and any association with other filter system is not yet available. Aims. We aim to edit complete visible to near infrared taxonomy and extend this work to any possible filters system. To do this, we generate mean spectra for each individual group, from a data set of 43 spectra. This work also presents new spectra of the TNO (38628) Huya, on which aqueous alteration has been suspected, and the Centaur 2007 VH305. -
Mercury's Resonant Rotation from Secular Orbital Elements
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Institute of Transport Research:Publications Mercury’s resonant rotation from secular orbital elements Alexander Stark a, Jürgen Oberst a,b, Hauke Hussmann a a German Aerospace Center, Institute of Planetary Research, D-12489 Berlin, Germany b Moscow State University for Geodesy and Cartography, RU-105064 Moscow, Russia The final publication is available at Springer via http://dx.doi.org/10.1007/s10569-015-9633-4. Abstract We used recently produced Solar System ephemerides, which incorpo- rate two years of ranging observations to the MESSENGER spacecraft, to extract the secular orbital elements for Mercury and associated uncer- tainties. As Mercury is in a stable 3:2 spin-orbit resonance these values constitute an important reference for the planet’s measured rotational pa- rameters, which in turn strongly bear on physical interpretation of Mer- cury’s interior structure. In particular, we derive a mean orbital period of (87.96934962 ± 0.00000037) days and (assuming a perfect resonance) a spin rate of (6.138506839 ± 0.000000028) ◦/day. The difference between this ro- tation rate and the currently adopted rotation rate (Archinal et al., 2011) corresponds to a longitudinal displacement of approx. 67 m per year at the equator. Moreover, we present a basic approach for the calculation of the orientation of the instantaneous Laplace and Cassini planes of Mercury. The analysis allows us to assess the uncertainties in physical parameters of the planet, when derived from observations of Mercury’s rotation. 1 1 Introduction Mercury’s orbit is not inertially stable but exposed to various perturbations which over long time scales lead to a chaotic motion (Laskar, 1989). -
SATELLITES ORBIT ELEMENTS : EPHEMERIS, Keplerian ELEMENTS, STATE VECTORS
www.myreaders.info www.myreaders.info Return to Website SATELLITES ORBIT ELEMENTS : EPHEMERIS, Keplerian ELEMENTS, STATE VECTORS RC Chakraborty (Retd), Former Director, DRDO, Delhi & Visiting Professor, JUET, Guna, www.myreaders.info, [email protected], www.myreaders.info/html/orbital_mechanics.html, Revised Dec. 16, 2015 (This is Sec. 5, pp 164 - 192, of Orbital Mechanics - Model & Simulation Software (OM-MSS), Sec 1 to 10, pp 1 - 402.) OM-MSS Page 164 OM-MSS Section - 5 -------------------------------------------------------------------------------------------------------43 www.myreaders.info SATELLITES ORBIT ELEMENTS : EPHEMERIS, Keplerian ELEMENTS, STATE VECTORS Satellite Ephemeris is Expressed either by 'Keplerian elements' or by 'State Vectors', that uniquely identify a specific orbit. A satellite is an object that moves around a larger object. Thousands of Satellites launched into orbit around Earth. First, look into the Preliminaries about 'Satellite Orbit', before moving to Satellite Ephemeris data and conversion utilities of the OM-MSS software. (a) Satellite : An artificial object, intentionally placed into orbit. Thousands of Satellites have been launched into orbit around Earth. A few Satellites called Space Probes have been placed into orbit around Moon, Mercury, Venus, Mars, Jupiter, Saturn, etc. The Motion of a Satellite is a direct consequence of the Gravity of a body (earth), around which the satellite travels without any propulsion. The Moon is the Earth's only natural Satellite, moves around Earth in the same kind of orbit. (b) Earth Gravity and Satellite Motion : As satellite move around Earth, it is pulled in by the gravitational force (centripetal) of the Earth. Contrary to this pull, the rotating motion of satellite around Earth has an associated force (centrifugal) which pushes it away from the Earth. -
Atmospheres and Surfaces of Small Bodies and Dwarf Planets in the Kuiper Belt
EPJ Web of Conferences 9, 267–276 (2010) DOI: 10.1051/epjconf/201009021 c Owned by the authors, published by EDP Sciences, 2010 Atmospheres and surfaces of small bodies and dwarf planets in the Kuiper Belt E.L. Schallera Lunar and Planetary Laboratory, University of Arizona, Tucson, AZ 85721, USA Abstract. Kuiper Belt Objects (KBOs) are icy relics orbiting the sun beyond Neptune left over from the planetary accretion disk. These bodies act as unique tracers of the chemical, thermal, and dynamical history of our solar system. Over 1000 Kuiper Belt Objects (KBOs) and centaurs (objects with perihelia between the giant planets) have been discovered over the past two decades. While the vast majority of these objects are small (< 500 km in diameter), there are now many objects known that are massive enough to attain hydrostatic equilibrium (and are therefore considered dwarf planets) including Pluto, Eris, MakeMake, and Haumea. The discoveries of these large objects, along with the advent of large (> 6-meter) telescopes, have allowed for the first detailed studies of their surfaces and atmospheres. Visible and near-infrared spectroscopy of KBOs and centaurs has revealed a great diversity of surface compositions. Only the largest and coldest objects are capable of retaining volatile ices and atmospheres. Knowledge of the dynamics, physical properties, and collisional history of objects in the Kuiper belt is important for understanding solar system formation and evolution. 1 Introduction The existence of a belt of debris beyond Neptune left over from planetary accretion was proposed by Kuiper in 1951 [1]. Though Pluto was discovered in 1930, it took over sixty years for other Kuiper belt objects (KBOs) to be detected [2] and for Pluto to be recognized as the first known member of a larger population now known to consist of over 1000 objects (Fig. -
2. Orbital Mechanics MAE 342 2016
2/12/20 Orbital Mechanics Space System Design, MAE 342, Princeton University Robert Stengel Conic section orbits Equations of motion Momentum and energy Kepler’s Equation Position and velocity in orbit Copyright 2016 by Robert Stengel. All rights reserved. For educational use only. http://www.princeton.edu/~stengel/MAE342.html 1 1 Orbits 101 Satellites Escape and Capture (Comets, Meteorites) 2 2 1 2/12/20 Two-Body Orbits are Conic Sections 3 3 Classical Orbital Elements Dimension and Time a : Semi-major axis e : Eccentricity t p : Time of perigee passage Orientation Ω :Longitude of the Ascending/Descending Node i : Inclination of the Orbital Plane ω: Argument of Perigee 4 4 2 2/12/20 Orientation of an Elliptical Orbit First Point of Aries 5 5 Orbits 102 (2-Body Problem) • e.g., – Sun and Earth or – Earth and Moon or – Earth and Satellite • Circular orbit: radius and velocity are constant • Low Earth orbit: 17,000 mph = 24,000 ft/s = 7.3 km/s • Super-circular velocities – Earth to Moon: 24,550 mph = 36,000 ft/s = 11.1 km/s – Escape: 25,000 mph = 36,600 ft/s = 11.3 km/s • Near escape velocity, small changes have huge influence on apogee 6 6 3 2/12/20 Newton’s 2nd Law § Particle of fixed mass (also called a point mass) acted upon by a force changes velocity with § acceleration proportional to and in direction of force § Inertial reference frame § Ratio of force to acceleration is the mass of the particle: F = m a d dv(t) ⎣⎡mv(t)⎦⎤ = m = ma(t) = F ⎡ ⎤ dt dt vx (t) ⎡ f ⎤ ⎢ ⎥ x ⎡ ⎤ d ⎢ ⎥ fx f ⎢ ⎥ m ⎢ vy (t) ⎥ = ⎢ y ⎥ F = fy = force vector dt -
Way-Out World
Non-fiction: Way-Out World Way-Out World By Hugh Westrup What strange satellite circles the visible edge of the solar system? The detonation of a single nuclear bomb can do catastrophic damage. So imagine the power of more than one bomb—not just two or 10 or even 10 million, but 10 billion. Astronomers have evidence that a collision with enough force to equal the explosion of 10 billion nuclear bombs once happened in the solar system. Out of that crack-up was born one of the oddest things in space. Its name is Haumea. “There is so much to learn about this newfound object, and we keep finding surprises,” says Mike Brown, an astronomer at the California Institute of Technology. “It’s just crazy.” ODD Balls The solar system is always changing. What astronomers know about it is changing even faster. Advances in telescope technology keep deepening their view of space, continually revealing new objects and new features on old objects. One example of that change in perspective is Pluto. For more than 70 years, astronomers considered it the ninth planet. Then, in 2007, the International Astronomical Union reclassified it as a dwarf planet. Like a planet, a dwarf planet orbits the sun. It also has enough mass, and therefore enough gravity, to give it a rounded shape. But it lacks pull; its gravity isn’t strong enough to clear its neighborhood of most smaller objects the way that planets do. A year later Pluto was reclassified again. Now it’s a plutoid. A plutoid is simply a dwarf planet that exists beyond Neptune, the eighth planet. -
Ice Ontnos: Focus on 136108 Haumea
Ice onTNOs: Focus on 136108 Haumea C. Dumas Collaborators: A. Alvarez, A. Barucci, C. deBergh, B. Carry, A. Guilbert, D. Hestroffer, P. Lacerda, F. deMeo, F. Merlin, C. Snodgrass, P. Vernazza, … Haumea Pluto (dwarf planets) DistribuTon of TNOs Largest TNOs Icy bodies in the OPSII context • Reservoir of volales in the solar system (H2O, N2, CH4, CO, CO2, C2H6, NH3OH, etc) • Small bodies populaon more hydrated than originally pictured – Main-belt comets (Hsieh and JewiZ 2006) – Themis asteroids family (Campins et al. 2010, Rivkin and Emery 2010) • Transport of water to the inner terrestrial planets (e.g. talk by Paul Hartogh) Paranal Observatory 6 SINFONI at UT4 7 SINFONI + NACO at UT4 8 SINFONI = MACAO + SPIFFI (SINFONI=Spectrograph for INtegral Field Observations in the Near Infrared) • AO SYSTEM: MACAO (Multi-Application Curvature Adaptive Optics): – Similar to UTs AO system for VLTI – 60 elements curvature sensing bimorph mirror – NGS or LGS – Developed by ESO • NEAR-IR SPECTRO: SPIFFI (SPectrometer for Infrared Faint Field Imaging): – 3-D spectrograph, 32 image slices, 1-2.5µm – Developed by MPE:Max Planck Institute for Extraterrestrial Physics + NOVA: Netherlands Research School for Astronomy SINFONI - Main characteristics • Location UT4 Cassegrain • Wavelength range 1-2.5µm • Detector 2048 x 2048 HAWAII array • Gratings J,H,K,H+K • Spectral resolution 1500 (H+K-filter) to 4000 (K-band) (outside OH lines) • Limiting magnitude (0.1”/spaxel) K~18.2, H+K~19.2 in hr, SNR~10 • FoV sampling 32 slices • Spatial resolution 0.25”/slice (no-AO), 0.1”(AO), 0.025” (AO) • Resulting FoV 8”x8”, 3”x3”, 0.8”x0.8” • Modes noAO, NGS-AO, LGS-AO SINFONI - IFS Principles SINFONI - IFS Principles (Cont’d) SINFONI - products Reconstructed image PSF spectrum H+K TNOs spectroscopy Orcus (Carry et al.