Deep stall aircraft landing

Patent metadata

Field	Value
Publication number	US-9208689-B2
Application number	US-201213261814-A
Country	US
Kind code	B2
Filing date	Aug 16, 2012
Priority date	Aug 19, 2011
Publication date	Dec 8, 2015
Grant date	Dec 8, 2015

Abstract

An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.

First claim

What is claimed is:

1. A method of rapidly descending an aircraft to land at a landing location, the aircraft having a wing including an upper surface and a lower surface defining an upright orientation for normal aircraft flight, and an inverted orientation for inverted flight, the upper surface being gravitationally above the lower surface while in the upright orientation, and the lower surface being gravitationally above the upper surface while in the inverted orientation, comprising:
(a) controlling the operation of one or more control surfaces to approach the landing location while the aircraft is flying in the upright orientation;
(b) controlling the operation of the one or more control surfaces to invert the aircraft such that it is controllably moving in an inverted orientation;
(c) controlling the operation of the one or more control surfaces to at least partially stall the wing while in the inverted orientation to provide for the aircraft to rapidly descend; and
(d) estimating the altitude of the aircraft by (1) estimating the rate of descent, (2) monitoring an image of the ground, and (3) calculating an estimated altitude using a rate of change of the monitored ground image and the estimated rate of descent.

2. A method of rapidly descending an aircraft to land at a landing location, the aircraft having a wing including an upper surface and a lower surface defining an upright orientation for normal aircraft flight, and an inverted orientation for inverted flight, the upper surface being gravitationally above the lower surface while in the upright orientation, and the lower surface being gravitationally above the upper surface while in the inverted orientation, wherein the aircraft uses a propeller for propulsion, comprising:
(a) controlling the operation of one or more control surfaces to approach the landing location while the aircraft is flying in the upright orientation;
(b) controlling the operation of the one or more control surfaces to invert the aircraft such that it is controllably moving in an inverted orientation;
(c) controlling the operation of the one or more control surfaces to at least partially stall the wing while in the inverted orientation to provide for the aircraft to rapidly descend; and
(d) stopping and maintaining the propeller in a substantially horizontal orientation prior to the aircraft reaching the landing location.

3. An unmanned aircraft system, comprising:
an aircraft including a wing having an upper surface and a lower surface defining an upright orientation for normal aircraft flight and an inverted orientation for inverted flight, the upper surface being gravitationally above the lower surface while in the upright orientation, and the lower surface being gravitationally above the upper surface while in the inverted orientation, and further including one or more control surfaces;
a remote-control station; and
a remote-control control system configured for a user to remotely control the flight of the aircraft using the remote-control station;
wherein the remote-control station is provided with an auto-land function that instructs the control system to automatically control the one or more control surfaces such that the aircraft conducts an inverting maneuver in which the aircraft rotates from the upright orientation to the inverted orientation, and such that the wing is at least partially stalled while the aircraft is in the inverted orientation; and
wherein the control system is configured to estimate the rate of descent, monitor a real-time image of the ground, and calculate an estimated altitude using a rate of change of the monitored ground image and the estimated rate of descent.

4. An unmanned aircraft system, comprising:
an aircraft including a wing having an upper surface and a lower surface defining an upright orientation for normal aircraft flight and an inverted orientation for inverted flight, the upper surface being gravitationally above the lower surface while in the upright orientation, and the lower surface being gravitationally above the upper surface while in the inverted orientation, and further including one or more control surfaces;
a remote-control station;
a remote-control control system configured for a user to remotely control the flight of the aircraft using the remote-control station; and
a propeller configured for propulsion of the aircraft;
wherein the remote-control station is provided with an auto-land function that instructs the control system to automatically control the one or more control surfaces such that the aircraft conducts an inverting maneuver in which the aircraft rotates from the upright orientation to the inverted orientation, and such that the wing is at least partially stalled while the aircraft is in the inverted orientation; and
wherein the control system is configured to stop the propeller and maintain it in a substantially horizontal orientation as a result of the auto-land function being activated.

Assignees

• Fisher Christopher E
• Szarek Thomas Robert
• Mcallister Justin B
• Belik Pavel
• Aerovironment Inc

Inventors

• Fisher Christopher E
• Szarek Thomas Robert
• Mcallister Justin B
• Belik Pavel

Classifications

• B64U2201/20

  Remote controls · CPC title

• B64U2201/00

  UAVs characterised by their flight controls · CPC title

• B64U2101/30

  for imaging, photography or videography · CPC title

• B64D31/00

  Power plant control systems; Arrangement of power plant control systems in aircraft · CPC title

• G08G5/54

  for approach or landing · CPC title