inertial measurement unit
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Inertial measurement unit — An inertial measurement unit, or IMU, is the main component of inertial guidance systems used in air , space , and watercraft, including guided missiles. An IMU works by sensing motion including the type, rate, and direction of that motion using… … Wikipedia
Inertial Measurement Unit — Ältere IMU in einer ballistischen Rakete Inertialsensoren (engl: Inertial Measurement Unit (IMU)) dienen zur Messung linearer Beschleunigungskräfte und Rotationskräften. Ein Inertialsensor besteht in der Regel aus drei Beschleunigungssensoren und … Deutsch Wikipedia
Miniature Inertial Measurement Unit (MIMU) — is an Inertial Measurement Unit (IMU) developed and built by Honeywell International to control and stabilize spacecraft during mission operations. MIMUs can also be configured to perform as an Inertial Reference Unit (IRU). MIMUs have been flown … Wikipedia
Miniature inertial measurement unit (MIMU) — MIMU exploded view (From Marlim.com) Miniature inertial measurement unit (MIMU) is an inertial measurement unit (IMU) developed and built by Honeywell International[ … Wikipedia
Inertial Reference Unit — An Inertial Reference Unit (IRU) is a type of inertial sensor which uses only gyroscopes to determine a moving aircraft’s or spacecraft’s change in angular direction (referred to as delta theta or Δθ) over a period of time. Unlike the Inertial… … Wikipedia
Inertial navigation system — An Inertial Navigation System (INS) is a navigation aid that uses a computer and motion sensors to continuously track the position, orientation, and velocity (direction and speed of movement) of a vehicle without the need for external references … Wikipedia
Inertial Reference System — Ein Inertiales Navigationssystem (INS) bestimmt die eigene Position und Geschwindigkeit, ohne dass ein Bezug zur äußeren Umgebung erforderlich ist. Der Begriff Trägheitsnavigation ist synonym, da Bewegungen über die Massenträgheit bei… … Deutsch Wikipedia
Saturn V Instrument Unit — The Saturn V Instrument Unit is a ring shaped structure fitted to the top of the Saturn V rocket s third stage (S IVB) and the Saturn IB s second stage (S IVB). It was immediately below the SLA (Spacecraft/Lunar Module Adapter) panels that… … Wikipedia
Apollo PGNCS — The Apollo Primary Guidance, Navigation and Control System (PGNCS) (pronounced pings) was a self contained inertial guidance system that allowed Apollo spacecraft to carry out their missions when communications with Earth were interrupted, either … Wikipedia
Abkürzungen/Luftfahrt/E–K — Dies ist der dritte Teil der Liste Abkürzungen/Luftfahrt. Liste der Abkürzungen Teil 1 A A Teil 2 B–D B; C; D Teil 3 E K E … Deutsch Wikipedia
MISTRAM — Missile Trajectory Measurement System. MISTRAM (MISsile TRAjectory Measurement) was a high resolution tracking system used by the United States Air Force (and later NASA) to provide highly detailed trajectory analysis of rocket launches. A… … Wikipedia
