arXiv (All)
open access
Method for Constrained Computational Guidance and Control with Application to Hypersonic Entry
A method for constrained computation guidance and control is described. The method employs guidance updates by periodically re-solving a constrained optimal control problem. Feasibility of the optimal control problem is improved by preventing constraint violations in the perturbed system. Constraint
Conceptio Open Archive
Analyze & explore related research in Conceptio
Connect this record directly into your research workflow or AI agent. Explore citations across open repositories, query full text, and export structured proof bundles.
This document is indexed with metadata only: full text is not available in the archive for this record. Open the official source ↗
Related documents
- 3405 New Guidance Method on Aerodynamic Ascent Path#69437
- Optimal Control of 2D Navier--Stokes Equations with Constraints of Finite Codimension#1154872
- Stability, breadth and guidance#94994
- Fixed-Order Robust Controller Design by Convex Optimization Using Spectral Models#1100233
- On Coupling Constraints in Pessimistic Linear Bilevel Optimization#388224
Record · ID 997797
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Bring this data into your agent: Connect via MCP or API · 20 free credits to start · no card required
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive