Lenticular airship and associated controls
A system for controlling yaw associated with an airship may include one or more vertical control surfaces associated with the airship, a first power source and a second power source, each configured to provide a thrust associated with the airship, and a yaw control configured to receive an input indicative of a desired yaw angle. The system may further include a controller communicatively connected to the yaw control, the one or more vertical control surfaces, and the first and second power sources. The controller may be configured to receive an output signal from the yaw control corresponding to the desired yaw angle and to generate a control signal configured to modify a state associated with at least one of the one or more vertical control surfaces, the first power source, and the second power source, such that the airship substantially attains the desired yaw angle.
1. A system for displaying attitude information associated with an airship, the system comprising:
a first plurality of indicators arranged along a horizontal axis configured to display a representation of a roll angle associated with the airship;
a second plurality of indicators arranged along a vertical axis, the second plurality of indicators intersecting the first plurality of indicators at an intersection; and
a processor configured to:
determine an attitude associated with the airship; and
cause at least one indicator of the first plurality of indicators or the second plurality of indicators to respond based on the attitude, wherein the number of the first plurality of indicators which respond indicates the roll angle associated with the airship.
2. The system of claim 1 , wherein the first and second plurality of indicators comprise light emitting diodes.
3. The system of claim 2 , wherein the response comprises lighting at least one of the light emitting diodes.
4. The system of claim 1 , further comprising a position sensor configured to sense a position associated with the airship and provide a signal indicative of the airship position to the processor.
5. The system of claim 4 , wherein the processor is configured to determine the attitude based on the signal.
6. The system of claim 1 , wherein the attitude comprises a pitch angle and a roll angle.
7. The system of claim 1 , wherein the second plurality of indicators is configured to display a representation of a pitch angle associated with the airship.
8. The system of claim 1 , further comprising a centered indicator at the intersection having a color distinct from any other indicators of the first plurality of indicators and the second plurality of indicators.
9. The system of claim 8 , wherein the centered indicator has a white color, and the other indicators associated with the first plurality of indicators and the second plurality of indicators have one of a green color, amber color and/or red color.
10. The system of claim 1 , wherein the first plurality of indicators and the second plurality of indicators are arranged on a substantially transparent material forming a display.
11. The system of claim 10 , wherein the display is positioned within a gondola associated with the airship so as to be in a line-of-site of an operator.
12. The system of claim 10 , wherein the display is positioned on top of an instrument cluster in the gondola.
13. The system of claim 1 , wherein the system is configured to form a heads-up display.
14. A method for displaying attitude information associated with an airship, the method comprising:
receiving a signal indicative of an attitude associated with the airship;
determining an attitude associated with the airship based on the signal; and
causing at least one indicator of a first plurality of indicators and a second plurality of indicators to respond according to the attitude, the first plurality of indicators being arranged substantially along a horizontal axis, and the second plurality of indicators being arranged substantially along a vertical axis and intersecting the first plurality of indicators, wherein the number of the first plurality of indicators which respond indicates a roll angle associated with the airship.
15. The method of claim 14 , wherein the first and second plurality of indicators comprise light emitting diodes.
16. The method of claim 15 , wherein the causing of at least one indicator of a first plurality of indicators and a second plurality of indicators to respond according to the attitude comprises lighting at least one of the light emitting diodes.
17. The method of claim 14 , wherein the attitude comprises a pitch angle and a roll angle.
18. The method of claim 17 , wherein the first and second plurality of indicators comprise light emitting diodes and the causing of at least one indicator of a first plurality of indicators and a second plurality of indicators to respond according to the attitude comprises lighting at least one of the light emitting diodes of the first plurality of indicators to display a representation of the roll angle.
19. The method of claim 17 , wherein the first and second plurality of indicators comprise light emitting diodes and the causing of at least one indicator of a first plurality of indicators and a second plurality of indicators to respond according to the attitude comprises lighting at least one of the light emitting diodes of the second plurality of indicators to display a representation of the pitch angle.
20. The method of claim 17 , wherein a centered indicator at the intersection of the first plurality of indicators and the second plurality of indicators has a white color, and other indicators associated with the first plurality of indicators and the second plurality of indicators have one of a green color, amber color, and/or red color progressing in a direction away from the centered indicator.
21. The method of claim 17 , further comprising causing only a centered indicator at the intersection of the first plurality of indicators and the second plurality of indicators, to respond when a pitch angle and a roll angle associated with the airship are substantially equal to zero.
22. The method of claim 14 , wherein the first plurality of indicators and the second plurality of indicators are arranged on a substantially transparent material forming a display.
23. A system for displaying attitude information associated with an airship, the system comprising:
a sensor configured to sense an attitude associated with the airship and generate a corresponding sensor output;
a substantially transparent display;
a first plurality of indicators arranged along a horizontal axis of the display configured to display a representation of a roll angle associated with the airship;
a second plurality of indicators arranged along a vertical axis of the display, the second plurality of indicators intersecting the first plurality of indicators; and
a processor configured to:
determine an attitude associated with the airship based on the sensor output; and
cause at least one indicator of the first plurality of indicators to light according to the attitude, wherein the number of the first plurality of indicators which respond indicates the roll angle associated with the airship.