Vehicle based independent tracking system
First Claim
1. A vehicle based independent tracking system comprised of:
- An object orientation and positioning system comprising an inertial measurement means and a global positioning system means capable of determining real-time dynamic space, position and time information solutions of a vehicle from ground operation through geosyncronous orbit mission phases, including high dynamic environments in the vicinity of five thousand meters per second in velocity, 10 g in acceleration, and 10 g per second in differential acceleration during all mission phases nominal or not, said inertial measurement means and global positioning system means being located aboard said vehicle;
said global positioning system means and inertial measurement means connected with a microcontroller system means providing power and data flow orchestration within said vehicle based independent tracking system, said microcontroller system means containing gravity software algorithms and switches to autonomously detect life and property threatening non-nominal vehicle performance, and send appropriately responsive destruct commands to said vehicle upon said vehicle'"'"'s crossing of pre-determined three dimensional time, space and position information range safety limit lines residing in software, said microcontroller system means containing memory survivable in high dynamic impact scenarios in the vicinity of 100 g, said microcontroller system means also connected with a power means, a mission specific array of application sensor means, a checkout and monitoring system means, a telemetry transmission means, and a radiating antenna system means, said radiating telemetry transmission means communicating with a telemetry receiver means off-board said vehicle, said telemetry receiver means connected with a user data terminal means, whereby a user can remotely monitor and respond to real-time flight profile parameters of said vehicle during all mission phases.
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Accused Products
Abstract
As an improvement to the architecture, utility, efficiency and cost associated with the procurement, setup, and operation of a real-time tracking/autonomous destruct and data recovery system for vehicles capable of exhibiting great velocities, accelerations, and attitude rates during all mission phases. A vehicle based independent tracking system 10 consists of an on-board vehicle data tracking system 12, an on-board vehicle data transmission system 14, an off-board flight data monitoring system 16, and a remote computer setup/test system 18. An interface umbilical-a 82 interconnects on-board vehicle data tracking system 12 with on-board vehicle data transmission system 14 for real-time transmission of dynamic time, space and position information of rockets and like vehicles to off-board flight data monitoring system 16 during all mission phases via an RF communication interface 86. Remote computer setup/test system 18 interfaces with on-board vehicle data tracking system 12 via an interface umbilical-b 84 for complete system checkout prior to launch.
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Citations
6 Claims
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1. A vehicle based independent tracking system comprised of:
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An object orientation and positioning system comprising an inertial measurement means and a global positioning system means capable of determining real-time dynamic space, position and time information solutions of a vehicle from ground operation through geosyncronous orbit mission phases, including high dynamic environments in the vicinity of five thousand meters per second in velocity, 10 g in acceleration, and 10 g per second in differential acceleration during all mission phases nominal or not, said inertial measurement means and global positioning system means being located aboard said vehicle; said global positioning system means and inertial measurement means connected with a microcontroller system means providing power and data flow orchestration within said vehicle based independent tracking system, said microcontroller system means containing gravity software algorithms and switches to autonomously detect life and property threatening non-nominal vehicle performance, and send appropriately responsive destruct commands to said vehicle upon said vehicle'"'"'s crossing of pre-determined three dimensional time, space and position information range safety limit lines residing in software, said microcontroller system means containing memory survivable in high dynamic impact scenarios in the vicinity of 100 g, said microcontroller system means also connected with a power means, a mission specific array of application sensor means, a checkout and monitoring system means, a telemetry transmission means, and a radiating antenna system means, said radiating telemetry transmission means communicating with a telemetry receiver means off-board said vehicle, said telemetry receiver means connected with a user data terminal means, whereby a user can remotely monitor and respond to real-time flight profile parameters of said vehicle during all mission phases. - View Dependent Claims (2, 3, 4, 5, 6)
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Specification