Computer implemented aircraft simulation method and apparatus

• US 6,062,715 A
• Filed: 03/21/1997
• Issued: 05/16/2000
• Est. Priority Date: 03/21/1997
• Status: Expired due to Fees

• Current Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Original Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Inventors: Moody, Larry A.
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): LOPPNOW, MATTHEW CLAY
• Application Number:
  US08/821,434
• Time in Patent Office: 1,152 Days
• Field of Search: 434/45, 434/29, 434/49, 434/51, 434/35, 434/46, 434/59, 73/570, 73/579, 73/583, 73/865.6, 364/578
• US Class Current: 703/2
• CPC Class Codes: G09B 9/08 for teaching control of aircraft, e.g. Link trainer

Abstract

A flight simulator includes a central processing unit and a flight simulation environment controlled by the central processing unit for simulating the flight of an aircraft. The central processing unit is programmed to observe a full fidelity model of the aircraft in flight so as to extract pilot inputs and aircraft responses at each of successive time intervals. The central processing unit is further programmed to calculate a damping and an undamped natural frequency of the aircraft from the extracted pilot inputs and aircraft responses and to simulate the flight of the aircraft by applying the damping and undamped natural frequency to a second order transfer function.

Claims

1. A flight simulation apparatus comprising a central processing unit and a flight simulation environment controlled by said central processing unit for simulating the flight of an aircraft, said central processing unit being programmed to observe a full fidelity model of the aircraft in flight so as to extract pilot inputs and aircraft responses at each of successive time intervals, said central processing unit being further programmed to calculate a damping and an undamped natural frequency of the aircraft from the extracted pilot inputs and aircraft responses and to simulate the flight of the aircraft by applying the damping and undamped natural frequency to a second order transfer function.

2. A flight simulation apparatus as claimed in claim 1, wherein said central processing unit calculates the damping ζ

and the undamped natural frequency ω

of the aircraft in accordance with;

##EQU2## and where φ

denotes roll, φ

'"'"' denotes roll rate, φ

" denotes roll acceleration and δ

.sub.φ

denotes lateral stick deflection as observed from the full fidelity model.

3. A flight simulation apparatus as claimed in claim 2, wherein the second order transfer function is represented by:

space="preserve" listing-type="equation">φ

"+2ζ

ω

φ

'"'"'+ω

.sup.2 =δ

.sub.φ

4. A flight simulation method implemented by a central processing unit and a flight simulation environment controlled by said central processing unit for simulating the flight of an aircraft, said method comprising observing a full fidelity model of the aircraft in flight so as to extract pilot inputs and aircraft responses at each of successive time intervals, calculating a damping and an undamped natural frequency of the aircraft from the extracted pilot inputs and aircraft responses, and simulating the flight of the aircraft by applying the damping and undamped natural frequency to a second order transfer function.

5. A flight simulation method as claimed in claim 4, wherein the damping ζ

and the undamped natural frequency ω

of the aircraft are calculated in accordance with;

##EQU3## and where φ

denotes roll, φ

'"'"' denotes roll rate, φ

" denotes roll acceleration and δ

.sub.φ

denotes lateral stick deflection as observed from the full fidelity model.

6. A flight simulator as claimed in claim 5, wherein the second order transfer function is represented by:

space="preserve" listing-type="equation">φ

"+2ζ

ω

φ

'"'"'+ω

.sup.2 =δ

.sub.φ