Sensors - Part One

The sensor suites on the Gabriel class starship are some of the most sophisticated and flexible sensor packages ever deployed on a Federation starship. These sensors make the Matrix one of the most capable command and control platforms ever built.

There are three primary sensor systems aboard the Matrix. The first is the long-range sensor array located at the front of the Engineering hull. This package of high-power devices is designed to sweep far ahead of the ships flight path to gather navigational, scientific and tactical information.

The second major sensor group is the lateral sensor arrays. These include the forward, port, starboard arrays on the rim of the Primary hull, as well as the port, starboard, and aft arrays on the Engineering hull and Carrier Bays. Additionally, there are smaller upper and lower sensor arrays near decks 2 and 12 on the Primary hull, providing coverage in the lateral arrays' blind spots.

The final major group is the navigational sensors. These dedicated sensors are tied directly into the ship's Flight Control systems and are used to determine the ship's location and velocity. They are located on the forward, upper port, upper starboard, aft, and upper and lower arrays.

In addition, there are several packages of special-purpose and engineering sensors such as the sub-space flow sensors, located at various points on the ship's hull.

The scientific sensor systems provide the Matrix and its crew with extensive capabilities in areas including:

Astronomical Observation – This includes optical and wideband EM scanning capabilities for the study of stellar objects and other phenomena across light year range. Capabilities include wide-angle scan ability for automated star-mapping functions and a wide range of individually
controlled instruments for mission-specific studies.

Planetary Surface Analysis – A broad range of short-range sensors provide extensive mapping and survey capabilities from planetary orbit. Besides high-resolution optical and EM scanning, virtual neutrino spectrometers and short-range quark resonance scanners provide detailed geologic structure analysis.

Remote Lifeform Analysis – A sophisticated array of charged cluster quark resonance scanners provide detailed biological data across orbital
distances. When used in conjunction with optical and chemical analysis sensors, the lifeform analysis software is typically able to extrapolate a
bioform's gross structure and deduce the basic chemical composition.

Long-Range Sensors

The most powerful scientific instrument aboard the USS Matrix are probably those located in the long-range sensor array. This cluster of high-power active and passive subspace frequency sensors is located in the Engineering hull directly behind the main deflector dish.

The majority of instruments in the long-range array are active scan subspace devices, which permits information gathering at speeds greatly exceeding light. Maximum effective range of this array is approximately five light years in high-resolution mode. Operation in medium-to-low
resolution mode yields a useable range of approximately 17 light years (depending on instrument type). At this range, a sensor scan pulse transmitted at warp 9.9997 would take approximately forty-five minutes to reach its destination and another forty-five minutes to return to the
Matrix. Standard scan protocols permit comprehensive study of approximately one adjacent sector per day at this rate. Within the confines of a solar system, the long-range sensor array is capable of providing nearly instantaneous information.

Primary Instruments in the Long-Range array include:

Wide-Angle active EM Scanner
Narrow-Angle active EM Scanner
2.0 meter diameter Gamma Ray Telescope
Variable frequency EM Flux Sensor
Lifeform analysis instrument cluster
Parametric Subspace field strss sensor
Gravametric distortion scanner
Passive neutrino imaging scanner
Thermal imaging array

These devices are located in a series of eight instrument bays directly behind the main deflector dish on decks 18-22. Direct power taps from the EPS conduits are available for high-power instruments such as the passive neutrino scanner. The main deflector emitter screen includes perforated zones designed to be transparent for sensor use, although the subspace field stress and gravimetric distortion scanners cannot yield useful data when the deflector is operating at more than 55% of maximum rated power. Within these instrument bays, ten mount points are nominally unassigned and are available for mission specific or future upgrades. All instrumant bays share the use of the navigational deflector's three subspace field generators located on deck 22, providing the subspace flux potential allowing transmission of sensor impulses at warp speeds.

The long-range sensor array is designed to scan in the direction of flight, and it is routinely used to search for possible flight hazards such as
micrometeoroids or other debris. This operation is managed by the Flight Control Officer under automated control. When small particulates or other minor hazards are detected, the main deflector is automatically instructed to sweep the objects from the vehicle's flight path. The scan range and degree of deflection vary with the ship's velocity. In the event that larger objects are detected, automatic minor changes in the flight path can avoid potentially dangerous collisions. In such cases, the computer will notify the Flight Control Officer of the situation and offer the
opportunity for manual intervention if possible.

Sensors - Part Two

Navigational Sensors

The Matrix sensor system constantly process incoming sensor data and routinely performs billions of calculations each second in an effort to
mimic the biological solution to the problem of navigation. While an equivalent number of Matrix sensors and simulated neurons (and their interconnections) within the main computers are still many orders of magnitude less efficient design than a organic brain, nonetheless, the Matrix system is more than adequate to the task of traversing the galaxy.

Sensors provide the input; the navigational processors within the main computers reduce the incessant stream of impulses into usable position and velocity data. The specific navigational sensors being polled at any instant will depend on the current flight situation. If the starship is in
orbit about a known celestial object, such as a planet in a chartered system, many long-range sensors will be inhibited, and short-range devices
will be favored. If the ship is cruising in interstellar space, the long-range sensors are selected and a majority of the short-range sensors are powered down. As with an organic system, the computers are not overwhelmed by a barrage of sensory information.

The 250 navigational sensor assemblies are, by design, isolated from extraneous cross-links with other general sensor arrays. This isolation
provides more direct impulse pathways to the computers for rapid processing, especially during high warp factors, where minute directional errors, in hundredths of an arc-second per light year, could result in impact with a star, planet or asteroid. In certin situations, selected cross-links may be created in order to filter out system discrepancies flagged by the main computer.

Each standard suite of navigational sensors includes:

Quasar Telescope
Wide-Angle IR Source Tracker
Narrow-Angle IR-UV-Gamma Ray Imager
Passive Subspace Multibeacon Receiver
Stellar Graviton Detectors
High-Energy Charged Particle Detectors
Galactic Plasma Wave Cartographic Processor
Federation Timebase Beacon Receiver
Stellar Pair Coordinate Imager


The navigational system within the main computers accepts sensor input at adaptive data rates, mainly tied to the ship's true velocity within the
galaxy. The subspace fields within the computers, which maintain faster-than-light (FTL) processing, attempt to provide at least 30% higher proportional energies than those required to drive the spacecraft, in order to maintain a safe collision-avoidance margin. If the FTL processing power drops below 20% over propulsion, general mission rules dictate a commensurate drop in warp motive power to bring the safety level back up. Specific situations and resulting courses of action within the computer will determine the actual procedures, and special navigation operating rules are followed during emergency and combat conditions.

Sensor input processing algorithms take two distinct forms, baseline code and rewritable code. The baseline code consists of the latest version of 3D and 4D position and flight motion software, as installed during Starbase overhauls. This code resides within the protected archival computer core segments and allows the starship to perform all general flight tasks. The Matrix has undergone one complete and two partial reinstallations of its baseline code since its first spacedock departure. The rewriteable code can take the form of multiple revisions and translations of the baseline code into symbolic language to fit new scenarios and allow the main computers to create their own procedure solutions, or add to an existing database of proven solutions.

These solutions are considered to be learned behaviors and experiences, and are easily shared with other Starfleet ships as part of an overall
spacecraft species maturing process. They normally include a large number of predictive routines for high warp flight, which the computers use to compare predicted interstellar positions against realtime observations, and from which they can derive new mathematical formulae. A maximum of 1,024 complete switchable rewrite versions can reside in the main memory at one time, or a maximum of 12,665 switchable code segments. Rewritable navigation code is routinely downloaded during major Starbase layovers and transmitted or physically transferred to Starfleet for analysis.

Sensor pallets dedicated to navigation, as with certain tactical and propulsion systems, undergo preventative maintenance and swapout on a more frequent schedule than other science-related equipment, owing to the critical nature of their operation. Healthy components are normally removed after 60-70% of their established lifetimes. This allows additional time for component refurbishment, and a larger performance margin if swapout is delayed by mission conditions or periodic spare unavailability. Rare detector materials, or those hardware components requiring long manufacturing lead times, are found in the quasar telescope (shifted frequency aperture window and beam combiner focus array) wide angle IR source tracker (cryogenic thin-film fluid recirculator) and galactic plasma wave cartographic processor (fast Fourier transform subnet). A 6% spares supply exists for these devices, deemed acceptable for the foreseeable future. Compared to a 15% spares supply for other sensors.

Lateral Sensor Arrays

The Matrix is equipped with the most extensive array of sensor equipment available. The spacecraft exterior incorporates a number of large sensor arrays providing ample instrument positions and optimal three-axis coverage.

Each sensor array is composed of a continuous rack in which are mounted a series of individual sensor instrument pallets. These sensor pallets are modules designed for easy replacement and updating of instrumentation. Approximately two-thirds of all pallet positions are occupied by standard Starfleet science sensor packages, but the remaining positions are available for mission-specific instrumentation. Sensor array pallets provide microwave power feed, optical data net links, cryogenic coolant feeds, and mechanical mounting points. Also provided are four sets of instrumentation steering servo cluster and two data subprocessor computers.

The standard Starfleet science sensor complement consists of a series of
six pallets, which include the following devices:

Pallet #1
Wide-angle EM radiation imaging scanner
Quark population analysis counter
Z-range particulate spectrometry sensor


Pallet #2
High-energy proton spectrometry cluster
Gravimetric distortion mapping scanner


Pallet #3
Steerable lifeform analysis instrument cluster

Pallet #4
Active magnetic interferometry scanner
Low-frequency EM flux sensor
Localized subspace field stress sensor
Parametric subspace field stress sensor
Hydrogen-filter subspace flux scanner
Linear calibration subspace flux sensor


Pallet #5
Variable band optical imaging cluster
Virtual aperture graviton flux spectrometer
High-resolution graviton flux spectrometer
Very low energy graviton spin polarimeter


Pallet #6
Passive imaging gamma interferometry sensor
Low-level thermal imaging sensor
Fixed angle gamma frequency counter
Virtual particle mapping camera


The standard Starfleet sensor complement comprises twenty-four-redundant suites of these six standard sensor pallets. These 144 pallets are
distributed on the Primary hull and Engineering hull lateral arrays. The instrumentation is located to maximize redundant coverage. A total of 244
pallet positions are available on both hulls.

The upper and lower sensor platforms provide coverage in very high and very low vertical elevation zones. These arrays employ a more limited subset of the standard Starfleet instrument packages.

In addition to standard Starfleet instruments, mission specific investigations frequently require nonstandard instruments that can be installed into one or more of the 100 nondedicated sensor pallets. When such devices are relatively small, such installation can be accomplished from access ports inside the spacecraft.

Installation of larger devices must be accomplished by extravehicular activity. A number of personnel airlocks are located in the sensor strip bays for this purpose. If a device is sufficiently large, or if installation entails replacement of one or more entire sensor pallets, a shuttlepod or workbee can be used for extravehicular equipment handling.

Copied in whole by - Lt.Cmdr. Wayne N Snyder
Date - 9811.07

Bibliography

Star Trek TNG Technical Manual – by R. Sternbach and M. Okuda

 

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