초록 ▼

One example embodiment relates to a navigation system for a guided projectile. The navigation system includes a detector within the guided projectile. The detector determines an actual amount of time it takes after launch for the guided projectile to accelerate through mach one. The navigation syste

One example embodiment relates to a navigation system for a guided projectile. The navigation system includes a detector within the guided projectile. The detector determines an actual amount of time it takes after launch for the guided projectile to accelerate through mach one. The navigation system further includes a guidance system within the object. The guidance system includes a projected flight plan for the guided projectile. The projected flight plan includes an estimated amount of time after launch it will take the object to accelerate through the speed of sound. The guidance system compares the actual amount of time and the estimated amount of time and adjusts the flight path of the guided projectile based on data received from the detector.

대표청구항 ▼

1. A navigation system for a guided projectile, the navigation system comprising: a detector within the guided projectile, wherein the detector determines an actual amount of time it takes after launch for the guided projectile to accelerate through mach one; anda guidance system within the object,

1. A navigation system for a guided projectile, the navigation system comprising: a detector within the guided projectile, wherein the detector determines an actual amount of time it takes after launch for the guided projectile to accelerate through mach one; anda guidance system within the object, wherein the guidance system includes a projected flight plan for the guided projectile, the projected flight plan including an estimated amount of time after launch it will take the object to accelerate through mach one, wherein the guidance system compares the actual amount of time and the estimated amount of time and adjusts the flight path of the guided projectile based on data received from the detector. 2. The navigation system of claim 1 wherein the detector determines an actual velocity that the guided projectile is traveling at as the guided projectile accelerates through mach one, and wherein the projected flight plan includes an estimated velocity that the guided projectile will be traveling at as the guided projectile accelerates through mach one, and wherein guidance system compares the actual velocity and the estimated velocity and adjusts the flight path of the guided projectile based on data received from the detector. 3. The navigation system of claim 2 wherein the detector determines the actual velocity that the guided projectile is traveling at as the guided projectile accelerates through mach one by determining a temperature of an environment that the guided projectile is traveling through. 4. The navigation system of claim 3 wherein the detector determines the actual velocity that the guided projectile is traveling at as the guided projectile accelerates through mach one by determining humidity, pressure and air density of the environment that the guided projectile is traveling through. 5. The navigation system of claim 1 wherein the detector is an inertial measurement unit that includes an accelerometer which measures acceleration of the guided projectile during flight. 6. The navigation system of claim 5 wherein the inertial measurement unit calculates jerk of the guided projectile during flight based on the measured acceleration of the guided projectile during flight. 7. The navigation system of claim 6 wherein the inertial measurement unit determines the actual amount of time it takes after launch for the guided projectile to accelerate through mach one based on the jerk of the guided projectile.