Abstract
A new model predictive convex programming is proposed in this paper for state and input constrained vehicle guidance design. The proposed method defines a convex optimization framework considering a flexibly designed cost function subject to inequality constraints and a sensitivity relation between state increments and input corrections. This formulated convex optimization problem can be solved in a computationally efficient manner. Simulation studies of nonlinear missile and aircraft landing guidance problems demonstrate the effectiveness of the proposed approach.
Original language | English |
---|---|
Article number | 8598772 |
Pages (from-to) | 2487-2500 |
Number of pages | 14 |
Journal | IEEE Transactions on Aerospace and Electronic Systems |
Volume | 55 |
Issue number | 5 |
DOIs | |
State | Published - Oct 2019 |
Keywords
- Aircraft landing
- constrained guidance
- missile guidance
- model predictive convex programming (MPCP)
- terrain constraints