BACKGROUND
Working in the space industry and coming across many instances of concerns, there seemed to be a need for such a visual self-checking wellbeing satellite and space vehicle monitoring system is controlled from a remote position.
EXAMPLES of some of the Materials used but not limited to:
Standard aluminum and cast Aluminum for track and arms and mounts
Rubber, compounds and carbon fiber suited for outer space with good outgassing characteristics
Electrically conductive wheels and wiring harnesses
Outgassing free epoxies, rubbers and plastics
Electrical circuit boards, electronic parts, such as diodes, capacitors, resistors, ASICs, analog and digital chips, wiring,
Miniature Cameras and optical lens and miniature microphones for audio sounds
DESCRIPTION OF DRAWINGS
FIG. 1 Artist rendition and illustration of the fully installed of the ASVVMS “Autonomous Space Vehicle Video Monitoring System”
FIG. 2 Drawing of “Modular Track System” (1) showing Track sections that can be configured and any mechanical layout
FIG. 2
a Fixed sections of the “Modular Track System”
FIG. 3 Drawing of main “Carriage and housing unit” mounts with wheels showing ASVVMS (3) Carriage housing including all controls and circuit boards, (4) Swivel joint for camera mount, (5) Driving Wheel, (6) Stabilizer Wheel, Transfers power to the Carriage unit, (7) Swivel joints
FIG. 4 Drawing of conductive section of the “Modular Track System”, (8) the tensioning system to ensure conductive contact to rails of the “Modular Track System”, (9) Outer Rails made of conductive material for electrical power transfer
FIG. 5 Drawing showing a single section of the “Modular Track System”, (9) Outer Rails made of conductive material for electrical power transfer, (10) Main rail made of non-conductive composite material, (11) The hollow Bracing fixture on bottom of Rail, (12) power cables, feeding electrical power to rails and transmitting and receiving all telemetry from the cameras
FIG. 6 Drawing showing electronics locations, (13) Interior space for circuit boards and control units, (14) Circuit Boards and control
FIG. 7 Drawing showing the Fixed Camera, (15) Surveillance Camera, (16) Fixed Mount
FIG. 8 Drawing showing the (4) rotation and Swivel Joints, (17) Camera extender and telescope arm in open position, (18) Extender Arm Joints, (15) Surveillance Camera, (1) Modular Track System, (3) Carriage Housing
FIG. 8A Drawing showing Rotating arm in closed position, (4) rotation and Swivel Joints, (17) Camera extender and telescope arm in open position, (18) Extender Arm Joints
DESCRIPTION OF OPERATION
The ASVVMS=Autonomous Space Vehicle Video Monitoring System is a robotic Autonomous and semi-autonomous camera system for the sole purpose of maintaining the Self-Health and Well-Being of the space vehicle it is mounted and designed onto. It is fixed on the structure of the Space Vehicle and can move on the “modular Track System” (CLAIM 2) that is custom fit to the space vehicle or satellite configurations. FIG. 1.
The Operation of the “Autonomous Space Vehicle Video Monitoring System” is achieved by manipulating from ground either a pre-programmed maneuver, or an autonomous maneuver in order to have the look over and project back to the operators on Earth what is happening with the space vehicle and satellite. Its primary mission being ensuring the health and wellbeing of the space vehicle or satellite it's affixed or flying on. CLAIM 1.
The ASVVMS moves along its “Modular Track System” (CLAIM 2) and looks for faulty areas or correctly functioning areas on the space vehicles and satellites. The Camera part of the system rides along the modular track and performs rotation to view in any 360 degree angle, in turn showing the performance of the space vehicle. By utilizing the ASVVMS, Autonomous Space Vehicle Video Monitoring System in FIG. 1, 4, 7, 8, the health and wellbeing will be maintained for the life of the space vehicle and satellite (CLAIM 1)
The wheels on the bottom of the “Carriage Device” (CLAIM 4) and camera run along the “Modular Track System” FIG. 2. (CLAIM 2, 3) on the space vehicle and satellite it is affixed to. The wheels are held solidly in place by force and tension which also provides electrical connectivity through the electrical sections of the tracks FIG. 2, FIG. 5. Additionally a wire harnesses runs internally FIG. 5.
The ASVVMS, Autonomous Space Vehicle Video Monitoring System moves around the space vehicle on the “Modular Track System” (FIG. 2, 3) either autonomously by being pre-programmed, uploaded via telemetry or manually real time operation. All of which is achieved visav the Integrated circuits or ASICS (FIG. 6) in the “Carriage Device” (CLAIM 4) and can be commanded from the ground via telemetry signal. During the movement around the pre-installed Modular track system FIG. 2, or manipulation of the camera head (FIG. 5, FIG. 7FIG. 8) the camera takes live video and audio and streams it live to those on the ground, or can be stored on its on board memory, then to be viewed. It can be stored on the on-board computer systems to be downloaded at a later time.
The ASVVMS in (FIG. 3, FIG. 7,) shows the aluminum, outgassing free composite and aluminum/aluminum alloy materials used for the housing which mounts directly to the tracks of the modular track system. It has connectivity via the electrically conductive wheels FIG. 3, underneath the housing with internal wiring FIG. 5.
Electrical conductivity is passed from the outer rails of the modular track system with conductive materials as well as internal wiring to the “main housing mount” in (FIG. 3, FIG. 5, FIG. 6) and diverted to the camera itself, then sending the communications signals to and from the ASVVMS.
The camera returns its video, Audio and telemetry signals back though the same systems via the internal wiring and conductive connections.
The ASVVMS=Autonomous Space Vehicle Video Monitoring System has a fixed mounting approach which has all the same functions, except in that it is fixed to one position on the space vehicle. It has the ability to be manipulated in any direction via the “Rotor Joints” FIG. 3, and also has the specific purpose of monitoring the health and wellbeing of the space vehicle (FIG. 7).
The electrical connections are made from within the “extender Arm” (FIG. 5, FIG. 8, FIG. 8A) up to the camera and back down the “Extender Arm” FIG. 8, the fixed connection and then it connects directly the space vehicle internal for telemetry and on board computer systems.
The “rotor joints” (FIG. 6, FIG. 7, FIG. 8) are configured and designed to have a 360 degree moving ability and made from aluminum and outgassing free Plastics, rubber and epoxies and composite type materials that are already approved for space use.
From the internal computer systems on board the space vehicles and satellites, the data from the ASVVMS, is sent back to the users, either on board the space vehicle with storage systems or in the air, or on the Earth, Space and ground.