OF THE
TIMES
The Authoritarian Follower believes that those in authority have the right to live by their own rules, and lying, cheating, stealing and murder in high places can thus be tolerated with a shrug of the shoulders. They will also willingly engage themselves in the same lying, cheating, stealing and murder if it is presented to them as necessary to protect their status quo.
Maybe the loud little handful ought to be subjected to higher level of scrutiny
The Hack War is now. U can keep your zeroes, All your ones are up for grabs.
Amazing how, after arriving here by trans dimensional and trans medium flight, once here they drive like it's the first day of snow on the roads...
overestimating their abilities in the water. Or underestimating the heart damage sustained by jabs.
Pavement Apes aren’t known to be strong swimmers.
To submit an article for publication, see our Submission Guidelines
Reader comments do not necessarily reflect the views of the volunteers, editors, and directors of SOTT.net or the Quantum Future Group.
Some icons on this site were created by: Afterglow, Aha-Soft, AntialiasFactory, artdesigner.lv, Artura, DailyOverview, Everaldo, GraphicsFuel, IconFactory, Iconka, IconShock, Icons-Land, i-love-icons, KDE-look.org, Klukeart, mugenb16, Map Icons Collection, PetshopBoxStudio, VisualPharm, wbeiruti, WebIconset
Powered by PikaJS 🐁 and In·Site
Original content © 2002-2026 by Sott.net/Signs of the Times. See: FAIR USE NOTICE

are becoming typical of science journalism in this, the 21st century. Meanwhile, Newton's laws remain unchanged.
Designing trajectories in a planet-moon environment using the controlled Keplerian map
Journal of Guidance, Control, and Dynamics 32(2), 436-443.
Piyush Grover and Shane D. Ross
Engineering Science and Mechanics, Virginia Polytechnic Institute and State University
[Link]
ABSTRACT
Designing fuel efficient trajectories which visit different moons of a planetary system is best handled by breaking up the problem into multiple three-body problems. This approach, called the patched three-body approach has received considerable attention in recent years, and has proved to lead to substantial fuel savings compared to the traditional patched-conic approach. We consider the problem of designing fuel-efficient multi-moon orbiter spacecraft trajectories in the Jupiter-Europa-Ganymede-spacecraft system with realistic transfer times. Fuel-optimal (i.e., near zero fuel) trajectories without using any control are first determined but turn out to be infeasible due to very long transfer times involved. We then describe a methodology which exploits the underlying structure of the dynamics of the two three-body problems, i.e., Jupiter-Europa-Spaceraft and Jupiter-Ganymede-Spacecraft, using the Hamiltonian structure-preserving Keplerian map approximations derived earlier and using small control inputs in the form of instantaneous Delta-Vs to get trajectories with times-of-flight on the order of months rather than several years. A typical trajectory constructed using the control algorithm can complete the mission in about 10% of the time-of-flight of an uncontrolled trajectory.