Applied receding horizon control of the caltech ducted fan

Proceedings of the American Control Conference

Volumn 5, Issue , 2002, Pages 3735-3740

  Franz, Ryan ^a   Milam, Mark ^b   Hauser, John ^a  

^a UCB 450   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

Guidance; Model predictive control; Nonlinear control; Optimal control; Real time optimization

Indexed keywords

COMPUTATIONAL METHODS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; DUCTED FAN ENGINES; LINEAR CONTROL SYSTEMS; LYAPUNOV METHODS; OPTIMAL CONTROL SYSTEMS; OPTIMIZATION; PREDICTIVE CONTROL SYSTEMS; STEP RESPONSE; SYSTEM STABILITY; UNMANNED VEHICLES;

CALTECH DUCTED FAN; INDOOR VECTORED THRUST FLIGHT; REAL-TIME OPTIMIZATION; RECEDING HORIZON CONTROL; SOFTWARE PACKAGE NTG;

NONLINEAR CONTROL SYSTEMS;

EID: 0036061484     PISSN: 07431619     EISSN: None     Source Type: Journal    
DOI: 10.1109/ACC.2002.1024508     Document Type: Article

References (10)

1. Model predictive control of a thrust-vectored flight control experiment
2. A lie-bäcklund approach to equivalence and flatness of non-linear systems
3. On the stability of unconstrained receding horizon control with a general terminal cost
4. Unconstrained receding-horizon control of nonlinear systems
5. Constrained model predictive control: Stability and optimality
6. A new computational approach to real-time trajectory generation for constrained mechanical systems
7. A testbed for nonlinear flight control techniques: The caltech ducted fan
8. Inversion based constrained trajectory optimization
9. Trajectory generation for a UAV in urban terrain, using nonlinear MPC