mean anomaly oor Masedonies
mean anomaly
en
An orbital parameter of a celestial body (in an elliptic orbit); the mean motion multiplied by the time since the last passage through periapsis; the angle PCM (measured in radians) defined by P = the periapsis, C = the center of the elliptical orbit, and M = the mean planet.
Vertalings in die woordeboek Engels - Masedonies
средна аномалија
en
one of the orbital elements used to specify the orbit of an object in space
Geskatte vertalings
Vertoon algoritmies gegenereerde vertalings
voorbeelde
Advanced filtering
Voorbeelde moet herlaai word.
Mean anomaly does not measure an angle between any physical objects.
Однесете гоWikiMatrix WikiMatrix
M0 is referred to as the mean anomaly at epoch, and t is the time since epoch.
Не, не е лоша идеја.Одлична идеја еWikiMatrix WikiMatrix
The mean anomaly is a mathematically convenient "angle" which varies linearly with time, but which does not correspond to a real geometric angle.
Се зборува дека се работи за реваншWikiMatrix WikiMatrix
Gaussian gravitational constant Kepler orbit Mean anomaly Mean longitude Orbital elements Do not confuse μ, the gravitational parameter with μ, the reduced mass.
Користи & анонимен пристапWikiMatrix WikiMatrix
The Keplerian elements are six: Inclination (i) Longitude of the ascending node (Ω) Argument of periapsis (ω) Eccentricity (e) Semimajor axis (a) Mean anomaly at epoch (M0).
За жал, верата не ни дозволуваWikiMatrix WikiMatrix
Because the rate of increase, n, is a constant average, the mean anomaly increases uniformly (linearly) from 0 to 2π radians or 0° to 360° during each orbit.
О. тоа е добро.Во мојата куќа е на друг начин. Ние тоа таму би го исчистилеWikiMatrix WikiMatrix
The mean anomaly is one of three angular parameters (known historically as "anomalies") that define a position along an orbit, the other two being the eccentric anomaly and the true anomaly.
Информации за корисници и лозинкиWikiMatrix WikiMatrix
If the mean anomaly is known at any given instant, it can be calculated at any later (or prior) instant by simply adding (or subtracting) n δt where δt represents the time difference.
Па, зар не ти се допаѓа?WikiMatrix WikiMatrix
The classical method of finding the position of an object in an elliptical orbit from a set of orbital elements is to calculate the mean anomaly by this equation, and then to solve Kepler's equation for the eccentric anomaly.
Знаеш, ти имаш сериозен проблемWikiMatrix WikiMatrix
9 sinne gevind in 5 ms. Hulle kom uit baie bronne en word nie nagegaan nie.