P. (1982), On the secular decrease in the semimajor axis of LAGEOS' orbit, Celestial Mech., 26, 361 - 382.Rubincam, D. P. (1982): On the Secular Decrease in the Semimajor Axis of Lageos's Orbit, Celest. Mech., 26, 361- 382....
分享到: 卫星轨道长半径 分类: 科技词汇|查看相关文献(pubmed)|免费全文文献 详细解释: 以下为句子列表: 分享到:
1) semi-major axis of satellite orbit 卫星轨道长半径2) satellite orbit 卫星轨道 1. The theoretical analysis and simulation result indicate that the satellite orbit and attitude changes have a great influence upon the space-borne SAR imaging. 理论分析与仿真结果表明卫星轨道近似与姿态变化对星载SAR...
publicvoidEllipticSector() {varo =newOrbit{ SemiMajorAxis =2, SemiMinorAxis =1, TransformAngle =0}; AssertAreClose(o.S(Math.PI),0); AssertAreClose(o.S(0),Math.PI); AssertAreClose(o.S(1, -Math.PI),2*Math.PI); } 开发者ID:dharco,项目名称:all-my-circuirs,代码行数:7,代码来源:...
semimajor axis, equivalent to the planet’s mean distance from the Sun. Theeccentricityof an elliptical orbit is a measure of the amount by which it deviates from a circle; it is found by dividing the distance between the focal points of the ellipse by the length of the major axis. To ...
Semimajor axis (a)— The sum of the periapsis and apoapsis distances divided by 2. Periapsis is the point at which an orbiting object is closest to the center of mass of the body it is orbiting. Apoapsis is the point at which an orbiting object is farthest away from the center of mass...
1.2 Eccentricity 1.3 Inclination 1.4 Semi-major axis 2 Types of orbits 2.1 Low Kerbin orbit (LKO) 2.2 Stationary orbit and synchronous orbit 2.3 Kerbisynchronous Equatorial Orbit (KEO) 2.4 Other 2.5 Suborbital 3 Orbits in the save file 3.1 Reference code 4 Notes 5 External linksProperties...
In general, the semimajor axis is along the y-axis with a value of a=2(C32+C42) and semiminor axis b=a2 meaning that the amplitude of the along-track relative motion is twice the radial one. The interesting result is that, regardless of the initial condition, the relative elliptical o...
The semimajor axis of the Lageos satellite's orbit is decreasing secularly at the rate of 1.1 mm day −1 . Ten possible mechanisms are investigated to discover which one (s), if any, might be causing the orbit to decay. Six of the mechanisms, resonance with the Earth's gravitational ...
the semimajor axis of the Hohmann transfer is one-half of the sum of the radii of the two circular orbits. Knowledge of the Hohmann transfer semimajor axis allows computation of the transfer time and the required velocities at each apse of the ellipse. Two velocity increments (Δv1and Δv2...