Thermal air data (TAD) system

Patent metadata

Field	Value
Publication number	US-9702892-B1
Application number	US-201414549665-A
Country	US
Kind code	B1
Filing date	Nov 21, 2014
Priority date	Nov 21, 2014
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

Embodiments relate to a system and vehicle for controlling the flight of a vehicle without the need to use pressure sensors. The system includes a plurality of pairwise thermal air data (TAD) sensors being controlled to have a constant temperature during heat dissipation into the atmosphere by each sensor. The system includes at least one processor configured to measure power for maintaining the constant temperature to calculate an angle of attack, a sideslip and a free stream vehicle velocity at infinity to control flight of a vehicle.

First claim

I claim:

1. A system comprising:
a plurality of pairwise thermal air data (TAD) sensors being controlled to have a constant temperature during heat dissipation; and
at least one processor configured to measure power for maintaining the constant temperature to calculate an angle of attack, a sideslip and a free-stream vehicle velocity at infinity to control flight of a vehicle.

2. The system of claim 1 , wherein each TAD sensor comprises:
a heat dissipating plate including a first surface and a second surface, the heat dissipating plate having a temperature maintained at the constant temperature, the heat dissipating plate configured to be located at a first location with a first surface flush with an exterior surface of the vehicle;
a heater coupled to the heat dissipating plate, the heater configured to heat the heat dissipating plate to the constant temperature;
a plate temperature sensor coupled to the heat dissipating plate;
a heater controller coupled to the heater and the plate temperature sensor, the heater controller configured to control the heater so that the heat dissipating plate maintains the constant temperature; and
an ambient air temperature sensor configured to be located at a second location flush with the exterior surface of the vehicle and being paired with the first location.

3. The system of claim 2 , wherein the heater is a resistive heater and being in surface to surface contact with the second surface of the heat dissipating plate.

4. The system of claim 2 , wherein the heat dissipating plate is made of a material having a thermal conductivity above 24 Btu/(hr. ° F. ft.).

5. The system of claim 1 , further comprising a coating on the heat dissipating plate, wherein the coating is made of a material with low observability (LO) properties.

6. The system of claim 1 , wherein the vehicle includes a vehicle body and a longitudinal axis, the plurality of TAD sensors are spaced circumferentially around the vehicle body in parallel to the longitudinal axis.

7. The system of claim 1 , further comprising one or more calibration tables correlated with a MACH number, a velocity ratio and a conjugate heat transfer coefficient.

8. A vehicle comprising:
a vehicle body having an exterior surface and a longitudinal axis;
a plurality of pairwise thermal air data (TAD) sensors coupled circumferentially around the vehicle body in parallel with the longitudinal axis and being controlled to have a constant temperature during heat dissipation; and
at least one processor configured to measure power for maintaining the constant temperature to calculate an angle of attack, a sideslip and a free-stream vehicle velocity at infinity to control flight of the vehicle.

9. The vehicle of claim 8 , wherein each TAD sensor comprises:
a heat dissipating plate including a first surface and a second surface, the heat dissipating plate having a temperature maintained at the constant temperature, the heat dissipating plate located at a first location of the vehicle body with a first surface flush with the exterior surface of the vehicle body;
a heater coupled to the heat dissipating plate, the heater configured to heat the heat dissipating plate to the constant temperature;
a plate temperature sensor coupled to the heat dissipating plate;
a heater controller coupled to the heater and the plate temperature sensor, the heater controller configured to control the heater so that the heat dissipating plate maintains the constant temperature; and
an ambient air temperature sensor coupled at a second location flush with the exterior surface of the vehicle body and being paired with the first location.

10. The vehicle of claim 9 , wherein the heater is a resistive heater and being in surface to surface contact with the second surface of the heat dissipating plate.

11. The vehicle of claim 9 , wherein the heat dissipating plate is made of a material having a thermal conductivity above 24 Btu/(hr. ° F. ft.).

12. The vehicle of claim 9 , further comprising a coating on the heat dissipating plate, wherein the coating is made of a material with low observability (LO) properties.

13. The vehicle of claim 8 , further comprising one or more calibration tables correlated with a MACH number, velocity ratio and a conjugate heat transfer coefficient wherein the angle of attack, the sideslip and the free-stream vehicle velocity at infinity are based on at least one of the MACH number, the velocity ratio and the conjugate heat transfer coefficient.

14. The vehicle of claim 8 , wherein the plurality of TAD sensors are configured to reduce drag.

Assignees

• Lockheed Corp

Inventors

• Richardson Nathan R

Classifications

• G05D1/10

  Simultaneous control of position or course in three dimensions (G05D1/12 takes precedence) · CPC title

• G01P5/10

  by measuring thermal variables · CPC title

• B64D43/00

  Arrangements or adaptations of instruments · CPC title

• G01P13/025 Primary

  indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw · CPC title

• B64D43/02

  for indicating aircraft speed or stalling conditions · CPC title