Method and apparatus for satellite antenna pointing
    2.
    发明授权
    Method and apparatus for satellite antenna pointing 有权
    卫星天线指向的方法和装置

    公开(公告)号:US06956526B1

    公开(公告)日:2005-10-18

    申请号:US10967416

    申请日:2004-10-18

    CPC分类号: H01Q19/12 H01Q1/1257 H01Q3/08

    摘要: A method of pointing an antenna at a transmitter comprising the steps of: (a) varying the azimuth of the antenna dish a predetermined number of degrees in a first direction from a predetermined azimuth angle; (b) measuring a first signal strength of an incoming signal received by the antenna dish; (c) varying the azimuth of the antenna dish the same predetermined number of degrees in a second direction from the predetermined azimuth angle, where the second direction is opposite to the first direction; (d) measuring a second signal strength of the incoming signal received by the antenna dish; and (e) comparing the first signal strength to the second signal strength, and if the first signal strength substantially equals the second signal strength, the current predetermined azimuth angle represents the optimal angle of azimuth for the antenna dish. However, if the first signal strength does not substantially equal the second signal strength, the process further comprises the steps of: (f) adjusting the predetermined azimuth angle, and (g) repeating steps (a)–(e). The same process is then repeated for the elevation adjustment.

    摘要翻译: 一种将天线指向发射机的方法,包括以下步骤:(a)从预定的方位角,在第一方向上改变天线盘的方位角预定数量; (b)测量由天线盘接收的输入信号的第一信号强度; (c)从第二方向与第一方向相反的预定方位角,在第二方向上改变天线盘的方位角相同的预定角度; (d)测量由天线盘接收的输入信号的第二信号强度; 和(e)将第一信号强度与第二信号强度进行比较,并且如果第一信号强度基本上等于第二信号强度,则当前预定方位角表示天线盘的最佳方位角。 然而,如果第一信号强度基本上不等于第二信号强度,则该处理还包括以下步骤:(f)调整预定的方位角,和(g)重复步骤(a) - (e)。 然后对于高程调整重复相同的过程。

    Tracking Non-Geo Synchronous Orbit satellites on orbiting planes of regular motion patterns

    公开(公告)号:US11947023B2

    公开(公告)日:2024-04-02

    申请号:US17245301

    申请日:2021-04-30

    IPC分类号: G01S19/42 G01S19/14 H01Q3/02

    CPC分类号: G01S19/42 G01S19/14 H01Q3/02

    摘要: A system and method for tracking non-geo synchronous orbit satellites on orbiting planes of regular motion patterns. The method includes providing a first satellites moving in a direction descending in latitude in first orbital planes and a second satellites moving in a direction ascending in latitude in second orbital planes; steering an antenna to an antenna tilt φ from normal with a single axis mechanism lined up with a first axis; scanning, electronically, with a linear array at a scan angle ψ along a second axis; and locking to a signal from a handed-from satellite from the first satellites, where the first axis is angled from the second axis, the steering along the first axis and the scanning along the second axis jointly track the handed-from satellite, the first orbits seem parallel, the second orbits seem parallel, and the first orbits seem aligned with the antenna tilt φ. A handoff between the first satellites may use one of the second satellites as a steppingstone.

    Tracking Non-Geo Synchronous Orbit Satellites on Orbiting Planes of Regular Motion Patterns

    公开(公告)号:US20220128708A1

    公开(公告)日:2022-04-28

    申请号:US17245301

    申请日:2021-04-30

    IPC分类号: G01S19/42 G01S19/14

    摘要: A system and method for tracking non-geo synchronous orbit satellites on orbiting planes of regular motion patterns. The method includes providing a first satellites moving in a direction descending in latitude in first orbital planes and a second satellites moving in a direction ascending in latitude in second orbital planes; steering an antenna to an antenna tilt φ from normal with a single axis mechanism lined up with a first axis; scanning, electronically, with a linear array at a scan angle ψ along a second axis; and locking to a signal from a handed-from satellite from the first satellites, where the first axis is angled from the second axis, the steering along the first axis and the scanning along the second axis jointly track the handed-from satellite, the first orbits seem parallel, the second orbits seem parallel, and the first orbits seem aligned with the antenna tilt φ. A handoff between the first satellites may use one of the second satellites as a steppingstone.

    Mannich detergents for hydrocarbon fuels
    10.
    发明申请
    Mannich detergents for hydrocarbon fuels 有权
    Mannich碳氢燃料清洁剂

    公开(公告)号:US20070169408A1

    公开(公告)日:2007-07-26

    申请号:US11336037

    申请日:2006-01-20

    IPC分类号: C10L1/22

    摘要: New, highly effective Mannich detergents for use in hydrocarbon fuels are described which reduce engine deposits in spark and compression ignition internal combustion engines. They are Mannich condensation reaction products obtained from reacting: (i) a polyamine having a sterically-hindered primary amino group, (ii) a hydrocarbyl-substituted hydroxyaromatic compound, and (iii) an aldehyde. These Mannich detergent compounds may be dispersed in a liquid carrier to provide a fuel additive concentrate for hydrocarbon engine fuels which effectively control engine deposit formation in intake valves and also other engine regions such as port fuel injectors and combustion chambers.

    摘要翻译: 描述了用于碳氢化合物燃料的新的,高效的曼尼希洗涤剂,其减少火花和压缩点火内燃机中的发动机沉积物。 它们是从以下反应获得的曼尼期缩合反应产物:(i)具有空间位阻伯氨基的多胺,(ii)烃基取代的羟基芳族化合物和(iii)醛。 这些Mannich洗涤剂化合物可以分散在液体载体中以提供用于碳氢化合物发动机燃料的燃料添加剂浓缩物,其有效地控制进气门以及其它发动机区域(例如端口燃料喷射器和燃烧室)中的发动机沉积物形成。