Validating a HamiltonJacobi Approximation to Hybrid System Reachable Sets - PowerPoint PPT Presentation

1 / 34
About This Presentation
Title:

Validating a HamiltonJacobi Approximation to Hybrid System Reachable Sets

Description:

NASA Ames (Automated Air Traffic Management) Announcement: Hybrid Systems ... (used in control logic design: Test A/C F-15, T-33) B. Embedded Software Design ... – PowerPoint PPT presentation

Number of Views:109
Avg rating:3.0/5.0
Slides: 35
Provided by: ianm176
Category:

less

Transcript and Presenter's Notes

Title: Validating a HamiltonJacobi Approximation to Hybrid System Reachable Sets


1
(No Transcript)
2
Personnel
  • Investigators
  • Claire Tomlin, Stephen Boyd, David Dill
  • Research Associates
  • Haitham Hindi, Henny Sipma, Dusan Stipanovic
  • Graduate Students
  • Alexandre Bayen, Jung Soon Jang, Ian Mitchell,
    Meeko Oishi, Rodney Teo , Lin Xiao
  • Research Collaborators
  • Boeing OCP (David Corman, Jim Paunicka, Brian
    Mendel, Don Winter), NASA, Boeing CAG
  • UC Berkeley (Hybrid Systems, Reachable Set
    Computation)

3
(No Transcript)
4
Technology Transfer
  • Boeing (OCP)
  • NASA Ames, Honeywell Labs, Boeing CAG (777
    Autoland)
  • NASA Ames (Automated Air Traffic Management)

Announcement Hybrid Systems 2002 (HSCC
2002) Stanford University, March 25-27,
2002 Organizers Claire Tomlin and Mark
Greenstreet www.stanford.edu/group/hscc2002
5
Schedule
  • Tomlin group 1.30-3.00
  • Boyd group 3.00-4.00
  • Sipma/Dill group 4.00-4.30
  • Discussion 4.30-5.00

6
Project Objectives
  • Design of computational methods to analyze and
    control hybrid systems (Tomlin, Dill, Boyd)
  • Design of communications and control strategies
    for networked control systems (Boyd)
  • Embedded software realizations (Tomlin, Dill)
  • Applications to
  • Verification of autopilot logic
  • Multiple aircraft collision avoidance maneuver
    design
  • Multiple sensor localization

7
Project Objectives
A
Verification and control design using hybrid
systems
B
Embedded software design
8
Discrete Codes for Verification and Synthesis
1. A Discrete Game
unsafe set
(i,j)
Player 2
Player 1
9
Discrete Codes for Verification and Synthesis
unsafe set after 1 play
(i,j)
Player 2
Player 1
10
Discrete Codes for Verification and Synthesis
unsafe set after 2 plays
(i,j)
Player 2
Player 1
11
Discrete Codes for Verification and Synthesis
unsafe set after 2 plays
Fixed point
(i,j)
Player 2
Player 1
12
Continuous Dynamic Games
  • Approximation methods
  • Predicate abstraction
  • Extract a discrete transition graph from
    signs of and

Example
13
Continuous Codes for Verification and Synthesis
2. A Continuous Game
unsafe set
14
Continuous Codes for Verification and Synthesis
unsafe set
15
Continuous Codes for Verification and Synthesis
unsafe set
16
Continuous Codes for Verification and Synthesis
unsafe set
17
Continuous Codes for Verification and Synthesis
unsafe set
18
Continuous Codes for Verification and Synthesis
unsafe set
19
Continuous Codes for Verification and Synthesis
unsafe set
20
Continuous Codes for Verification and Synthesis
unsafe set
  • Compute the set of variables (aircraft positions,
    velocities ) for which for all control
    actions, the system can be driven into the unsafe
    set by uncertainty or disturbance.
  • Efficient data structures to represent sets
    EXTREMELY important.

21
Continuous Reachable Set Calculation
Computation provides, at each
Distance to boundary Vector pointing to boundary
Theorem Computing
where is the unique
Crandall-Evans-Lions viscosity
solution to
22
A. Hybrid Codes for Verification and Synthesis
glide slope
3. A Hybrid Game
altitude
flare
TOGA
capture
23
Hybrid Codes for Verification and Synthesis
glide slope
altitude
flare
TOGA
capture
24
Hybrid Codes for Verification and Synthesis
glide slope
altitude
flare
TOGA
capture
25
Hybrid Codes for Verification and Synthesis
glide slope
altitude
flare
TOGA
capture
26
Hybrid Codes for Verification and Synthesis
glide slope
altitude
flare
TOGA
capture
Implementation in Boeings Open Control Platform
(used in control logic design Test A/C F-15,
T-33)
27
B. Embedded Software Design
  • Process 1 GPS
  • gps_position
  • 1 Hz
  • data storage

embedded software
real time operating system
28
B. Embedded Software Design
  • Process 1 GPS
  • gps_position
  • 1 Hz
  • data storage
  • Process 2 control
  • gps_position
  • 20 Hz
  • data retrieval

embedded software
real time operating system
29
Ian Mitchell
y
y
x
30
Alexandre Bayen
31
Meeko Oishi
what the pilot sees
with Boeing CAG, NASA Ames
32
Jung Soon Jang
33
Dusan Stipanovic
34
Rodney Teo
control
estimator
estimator
control
estimator
control
Each aircraft broadcasts its estimated
state Analyze performance with respect to link
reliability
Write a Comment
User Comments (0)
About PowerShow.com